NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS COLLECTION

Box 1 Technical Notes

No. 464 A Complete Tank Test of a Model of a Flying-Boat Hull - N.A.C.A. Model No. 11
No. 470 A Complete Tank Test of a Model of a Flying-Boat Hull-N.A.C.A. Model No. 11A
No. 471 A Complete Tank Test of a Model of a Flying-Boat Hull-N.A.C.A. Model 16
No. 482 The Effect of Spray Strips on a Model of The P3M-1 Flying-Boat Hull
No. 504 Completes Tank Tests of Two Flying-Boat Hulls with Pointed Steps-N.A.C.A. Models 22-A and 35
No. 512 A Complete Tank Test of The Hull of the Sikorsky S-40 Flying Boat- American Clipper Class
No. 525 The Aerodynamic Drag of Flying-Boat Hull Models As Measured in the N.A.C.A. 20-Foot Wind Tunnel -I
No. 531 Tank Tests of Model 11-G Flying -Boat Hull
No. 535 The Effect of Depth of Step on the Water Performance of a Flying-Boat Hull Model N.A.C.A. Model 11-C
No. 538 A General Tank Test of N.A.C.A. Model 11-C Flying-Boat Hull, Including the Effect of Changing the Plan Form of the Step
No. 551 Tank Tests of Three Models of Flying-Boat Hulls of the Pointed-Step Type with Different Angles of Dead Rise-N.A.C.A. Model 35 Series
No. 557 Considerations of the Take -Off Proble
No. 563 Tank Tests of Models of Floats for Single-Float Seaplanes-First Series
No. 566 Tank Tests of Models of The NC Flying-Boat Hull- N.A.C.A. Model 44
No. 574 Tank Tests of Models of Flying Boat Hulls Having Logi Tudinal Steps
No. 576 Tank Tests of Model of The Hull of the Navy PB-1 Flying -Boat -N.A.C.A. Model 52
No. 580 A General Tank Test of a Model of the Hull of The British Singapore IIC Flying Boat
No. 590 Hydrodynamic Tests in The N.AC.A. Tank of a Model of The Hull of The Short Calcutta Flying Boat
No. 635 Tank Tests of A Model of One Hull of The SAVOIA S-55-X Flying Boat- N.A.C.A Model 46
No. 638 Tank Tests of Model 36 Flying-Boat Hull
No. 643 A Study of Flying-Boat Take-Off
No. 657 Tank Tests to Show the Effect of Rivet Heads on The Water Performance of a Seaplane Float
No. 648 The Increased in Frictional Resistance caused by various types of Rivet Heads as Determined by Tests of Planning Surfaces
No. 677 Tests of a Contra-Propeller for Aircraft
No. 681 A General Tank Test of a Model of the Hull of the P3M-1 Flying-Boat including a Special Working Chart for The Determination of Hull Performance
No. 777 Internal-Flow Systems for Aircraft
No. 858 A Comparison of the Results from General Tank Tests of 1/6-And 1/12 Full-Size Models of The British Singapore IIC Flying Boat
No. 976 Tests of Airfoils Designed to Delay the Compressibility Burble
No. 1008 Analyses and Modification of Theory for Impact of Seaplanes on Water
No. 1056 The Effects of Various Parameters on the Load at which Spray Enters the Propellers of a Flying-Boat
No. 1062 Tank Tests to Determine the Effort of Varying Design parameters of Planing-Tall Hulls I-Effect of Varying Length, Width, and Plan-Form Taper of Afterbody
No. 1057 General Tank Tests of a 1/10 Size Model of the Hull of the Boeing XPBB_1 Flying-Boat-Langley Tank Model 175

Box 2

No. 1091 An Analysis of the Main Spray Characteristics of some Full-Size Multiengine Flying Boats
No. Tank Tests to Determine the Effect of Varying Design Parameters of Planing-Tall Hulls II-Effect of Varying Depth of Step, Angle of Afterbody Keel, Length of Afterbody Chine, and Gross Load
No. No. 1182 A Collection of the Collapsed Results of General Tank Tests of Miscellaneous Flying-Boat Hull Models
No.1237 Tank Investigation of a Powered Dynamic Model of a Large Long-Range Flying Boat-Langley Tank Model 180
No. 1245 Summary of Lateral-Control Research
No. 1349 Performance and Ranges of Applications of Various Types of Aircraft Propulsion System
No. No. 1166 Variation of Hydrodynamic Impact Loads with Flight-Path Angle for a Prismatic Float at 0^0 and 3^0 Term and with a 221/2 ^0 angle of Dead Rise
No.1253 Comparison of Design Specifications with the actual static Transverse Stability of 25 Seaplanes
No. 1268 An Application of Statistical Data in the Development of Gust-Load Criterions
No. 1284 Investigation at low speed of the Logitudinal Stability Characteristics of a 60^o Swept-Back Tapered Low -Drag Wing
No. 1287 Flight Tests of an airplane Model with a 42^0 Swept-Back Wing in the Langley Free-Flight Tunnel
No. 1288 Flight Tests of An Airplane Model with a 62^0 Swept-Back Wing in the Langley Free-Flight Tunnel
No. 1290 Appreciation and and Determination of the Hydrodynamic Qualities of Seaplanes
No. 1294 Investigation of Effect of Span, Spanwise Location, and Chordwise Location of Spoilers on Lateral Control Characteristics of a Tapered Wing
No. 1307 Effect of Aerodynamic Refinement on the Aerodynamic Characteristics of a Flying-Boat Hull
No. 1305 Effect of Length-Beam Ratio on the Aerodynamic Characteristics of Flying-Boat Hull
No. 1306 Aerodynamic Characteristics of Three Planing-Tail Flying -Boat Hulls
No. Effect of Horizontal-Tail Position on the Hinge Moments of an Unbalanced Rudder in Attitudes Simulation Spin Conditions
No. 1261 Effect of Variables in Welding Technique on the Strength of Direct-Current Metal-Arc-Welded Joints in Aircraft Steel I-Static Tension and Bending Fatigue Tests of Joints in SAE 4130 Steel Sheet
No. 1301
A Method for Calculating the Heat Required for the Prevention of Fog Formations on the Inside Surfaces of Single-Panel Bullet-Resisting Windshields During Diving Flight
No. 1339 Wind-Tunnel Investigation of the Effect of Power and Flaps on the Static Longitudinal Stability and Control Characteristics of a Single-Engine High-Wing Airplane Model
No. 1356 An Investigation of Effects of Reversed-Typed Logitudinal Steps on Resistance and Spray Characteristics of a Flying-Boat Hull
No. 1384 A Review of Boundary -Layer Literature
No. 1394 Flight Investigation on a Fighter -Type Airplane of Factors which Affect the Loads and Load Distributions on the Vertical Tail Surfaces During Rudder Kicks and Fishtails
No. 1398 Solutions for Hydrodynamic impact Force and Response of a Two-Mass System with an Application to an Elastic Airframe

Box 3

No. 1670 Appreciation and Prediction of Flying Qualities
No. 1679 Flight Measurement of the Longitudinal Stability , Stalling, and Lift Characteristics of an Airplane Having a 35^0 Swept Back Wing without Slots and with 40-Percent-Span Slots and Comparison with Wind-Tunnel Data
No. 1571 Effect of Afterbody Length and Keel Angle on Minimum Depth of Step for Landing Stability and on Take-Off Stability of a Flying Boat
No. 1686 Effect of Length -Beam Ratio on Aerodynamic Characteristics of Flying-Boat Hulls without Wing Interference
No. 1719 Flight Measurement of Buffeting Tail Loads
No. 1728 Spray Characteristics of Four Flying-Boat Hulls as Affected by Length -Beam Ratio
No. 1779 Effects of Antispin Fillets and Dorsal Fins on the Spin and Recovery Characteristics of Airplanes as Determined from Free-Spining -Tunnel Tests
No. 1759 Effects of Compressibility on Normal-Force, Pressure , and Load Characteristics of a Tapered Wing of NACA 66-Series Airfoil Sections with Split Flaps
No. 1493 A Statistical Study of Wave Conditions at Four Open-Sea Localities in the North Pacific Ocean
No. 1796 Theoretical Analysis of Oscillations of a Towed Cable
No. 1804 Effect of Logitudinal Steps on Skipping Characteristics of PB2Y-6 Flying Boat
No. 1818 Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds
No. 1839 Some Theoretical Low-Speed Span Loading Characteristics of Swept Wings in Roll and Sideslip
No. 1881 Comparison of Pitching Moments obtained During Seaplane Landings with Values Predicted by Hydrodynamic Impact Theory
No. 1929 On the Stability of the Free Laminar Boundary Layer Between Parallel Streams
No. 1968 Flight Tests of the Hydrodynamic Characteristics of a Japanese "Emily" Flying Boat
No. 1570 Hydrodynamic Qualities of a Hypothetical Flying Boat with a Low-Drag Hull having a Length - Beam Ratio of 15
No. 1578 Frictions of Solid Films on Steel at High Sliding Velocities
No. 1573 Flight Measurements of the Flying Qualities of Five Light Airplanes
No. 1578 Wind-Tunnel Investigation of a Systematic Series of Modifications to a Flying- Boat Hull
No. 1605 Accuracy of Airspeed Measurements and Flight Calibration Procedures
No. 1592 Compressible Flow Tables for Air
No. 1431 Investigation of the Aileron and Tab of a Spring- Tab Lateral- Control System in the Langley 19-Foot Pressure Tunnel
No. 1437 Impact Theory for Seaplane Landings
No. 1468 Low-Speed Static Stability and Damping in Roll Characteristics of Some Swept and UnSwept Low-Aspect-Ratio Wings
No. 1477 Generalized Performance Comparison of Large Conventional, Tail-Boom, and Tailless Airplanes
No. 1259 A Graphical Method for Interplation of Hydrodynamic Characteristics of Specific Flying Boats from Collapsed Results of General Tests of Flying -Boat-Hull Models
No. 1516A Generalized Theoretical and Experimental Investigation of the Motions and Hydrodynamic Loads Experienced By V-Bottom Seaplanes During Steps-Landing Impacts
No. 1524 Take-Off Performance of Light Twin-Float Seaplanes
No. 1547 Tank Tests of Three Types of Afterbodies on A Flying-Boat Model with Basic Hull Length-Beam Ratio of 10.0
No. 1404 Collection of Test Data For Lateral Control with Full -Span Flaps
No. 1563 Effect of Partial Wing Lift in Seaplane Landing Impact

Box 4

No.1926 The Application of the Statistical Theory of Extreme Values to Guest-Load Problems
No. 1993 Icing-Protection Requirements for Reciprocating-Engine Induction Systems
No. 2015 Water Landing Investigation of a Model Having a Heavy Beam Loading and A 30^0 Angle of Dead Rise
No. 2063 A Comparison of Theoretical and Experimental Wing Bending Moments During Seaplane Landings
No. 2413 Flight Investigation of the Effect of Control Centering Springs on the Apparent Spiral Stability of a Personal-Owner Airplane
No. 2416 Theoretical Study of Some Methods for Increasing the Smoothness of Flight Through Rough Air
No. 2481 Hydrodynamic Characteristics of a Low-Drag, Planning-Tail Flying-Boat Hull
No. 2508 Landing Characteristics in waves of three Dynamic Models of Flying Boats
No. 2624 Flame Speeds of Methane-Air, Propane-Air, And Ethylene-Air Mixtures at Low Initial Temperatures
No. 2659 A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diaphragm
No. 2297 Effect of an Encrease in Angle of Dead Rise on the Hydrodynamic Characteristics of a High-Length -Beam -Ration Hull
No. 2489 Aerodynamic Characteristics of a Refined Deep-Step Planing-Tail Flying-Boat Hull with Various Forebody and Afterbody Shapes
No. 2698 Theoretical Analyses of Hydrodynamic Impact of a Prismatic Float having Freedom in Trim
No. 2762 Aerodynamic Characteristics of Three Deep-Step Planing-Tail Flying-Boat Hulls and a Transverse-Step Hull with Extended Afterbody
No. 2929 Experimental Investigation of The Effect of Rear-Fuselage Shape on Ditching Behavior
No. 2966 Propeller-Performance Charts for Transport Airplanes
No. 3182 Manual of the ICAO Standard Atmosphere Calcuolations by the NACA
No. 3236 Wind-Tunnel Studies of the Performance of Multirotor Configurations
No. 3313 Some Measurements of Atmospheric Turbulence Obtained From Flow-Directions Vanes Mounted on an Airplane
No. 3423 Method of Controlling Stiffness Properties of a Solid-Construction Model Wing
No. 3432 Circumferential Distribution of Propeller-Slipstream Total- Pressure Rise at one Radial Station of a Twin-Engine Transport Airplane
No. 3537 Helicopter Instrument Flight and Precision Maneuvers as Affected By Changes in Damping in Roll, Pitch, And Yaw
No. 3619 Effect of Carriage Mass Upon the Loads and Motions of a Prismatic Body During Hydrodynamic Impact
No. 3637 Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device For Personnel Airplanes
No. 3710 Preliminary Investigation of the Effects of External Wing Fuel Tanks on Ditching Behavior of a Sweptback-Wing Airplane
No. 3803 Band- Pass Shock and Vibration Absorbers for Application to Aircraft Landing Gear
No. 3903 An Experimental Hydrodynamic Investigation of the Inception of Vortex Ventilation
No. 4129 Analysis of Operational Airline Data to Show the Effects of Airborne Weather Radar on the Gust Loads and Operating Practices of Twin-Engine Short-Haul Transport Airplanes
No. 4184 Measurement of Static Presssure on Aircraft
No. 4194 Comparison of Hydrodynamic -Impact Acceleration and Response for Systems with Single and With Multiple Elastic Modes
No. 4251 An Experimental Investigation of Wake Effects on Hydro-Skis
No. 4291 An Evaluation of Effects of Flexibility on Wing Strains in Rough Air for A Large Swept-Wing Airplane By Means of Experimentally Determined Frequency-Response Functions with an Assessment of Random -Process Techniques Employed
No. 4294 Effects on Nose Shape and Spray Control Strips on Emergence and Planing Spray of Hydro-Ski Models

Box 5

No.ADNO8-07-61.1 Water Impact Pressure Measurement
No. 133 Design Development and Initial Tests of ONR Supercavitating Hydrofoil Boat
XCH-6
Grumman High Speed Hydrodynamic Laboratory
GE-173 Hydrofoil Boat Hull-Wave Impact Loads
Hydrodynamics Division Files
No. 9646 JRF-5 Auxiliary Spray Strip Test Results
No. 2903.42 Applied Loads for Water Conditions
No. DA 10-480.3 Investigation of Hydrofoil Flutter Final Report
No.Nonr-3616(00) Grumman Research Department
Str-Mar-100 Hydroelastic Effects on the Lift of High Speed Hydrofoils
No. 164 Grumman Research Department
XA-M51-041-1 Hydrodynamics Report Gumman 80 Knot Transiting Foil System for the Fresh I test Craft

Box 6

No. XAR-A-45 Experimental Study of High Speed Hydrofoils

Box 7

No. DA Nonr-3989.3 Hydrofoil Flutter Small Sweep Angle Investigation Final Report
Operational Testing and Evaluation of the Hydrofoil Seacraft Denison
Gumman Experimental Study of High-Speed Hydrofoils
No. XAR-A-45 Experimental Study of High Speed Hydrofoils

Box 1????

No. 858 A Comparison of the Results from General Tank Tests of 1/6-and 1/12 Full Size Models of The British Singapore IIC Flying Boat
No. 777 Internal Flow Sytems for Aircraft
No. 681 A General Tank Test of a Model of the Hull of the P3M-1 Flying Boat Including a Special Working Chart for the Determination of Hull Performance
No. 677 Tests of a Contra-Propeller for Aircraft
No. 648 The Increase in Frictional Resistance caused by Various Types of Rivet Heads as Determined by Tests of Planing Surfaces
No.557 Considerations of the Take-Off Problem
No. 551 Tank Test of Three Models of Flying-Boat Hulls of the Pointed-Step Type with Different Angles of Dead Rise-N.A.C.A. Model 35 Series
No.538 A General Tank Test of N. A.C.A. Model 11-C Flying Boat Hull, Including the Effect of Changing the Plan Form of the Step
No. 657 Tank Tests to Show the Effect of Rivet Heads on The Water Performance of a Seaplane Float
No.643 A Study of Flying -Boat Take-Off
No. 638 Tank Tests of Model 36 Flying-Boat Hull
No. 635 Tank Tests of a Model of One Hull of the SAVOIA S-55-X Flying Boat-N.A.C.A. Model 46
No. 590 Hydrodynamic Tests in the N.A.C.A. Tank of a Model of the Hull of the Short Calcuta Flying Boat
No. 580 A General Tank Test of a Model of the Hull of The British Singapore IIC Flying Boat
No. 576 Tank Tests of a Model of the Hull of the Navy PB-1 Flying-Boat -N.A.C.A. Model 52
No. 1057 General Tank Tests of a 1/10 size Model of the Hull of the Boeing XPBB-1 Flying Boat-Langley Tank Model 175
No.1062 Tank Tests to Determined the Effect of Varying Design Parameters of Planing-Tail Hulls I-Effect of Varying Length, Width, and Plan -Form Taper of Afterbody.
No. 1056 The Effects of Various Parameters on the Load at which Spray Enters the Propellers of a Flying Boat
No. 1008 Analysis and Modification of Theory for Impact of Seaplanes on Water
No. 976 Tests of Airfoils Designed to Delay the Compressibility Burble
No. 535 The Effect of Depth of Step on the Water Performance of a Flying- Boat Hull Model N.A.C.A. Model 11-c
No. 531 Tank Tests of Model 11-G Flying-Boat Hull
No. 525 The Aerodynamic Drag of Flying -Boat Hull Models as Measured in the N.A.C.A. 20 Feet Wind Tunnel -I
No. 512 A Complete Tank Test of the Hull of the Sikorsky S-40 Flying Boat -American Clipper Class
No. 504 Complete Tank Tests of 2 Flying-Boat Hulls with Pointed Steps- N.A.C.A. Models 22-A and 35
No. 482 The Effect of Spray Strips on a Model of the P3M-1 Flying-Boat Hull
No. 471 A Complete Tank Test of a Model of a Flying -Boat Hull-N.A.C.A. Model 16
No. 470 A Complete Tank Test of a Model of a Flying-Boat Hull- N.A.C.A. Model No. 11-A
No. 464 A Complete Tank Test of a Model of a Flying -Boat Hull- N.A.C.A. Model No. 11
No. 574 Tank Test of Models of Flying Boat Hulls having Longitudinal Steps
No. 566 Tank Tests of Model of the NC Flying-Boat Hull-N.A.C.A. Model 44
No. 563 Tank Tests of Model of Floats for Single-Float Seaplanes-First Series

Box8

No. DA M51-239.1 Dynamic Tests of the 1/4 Scale Models of The 80 Knot Transiting Strut-Foil Systems
No. 4577(00) Grumman Final Report Study of Hydrofoil Singing
No. 003-1 An Analysis of Air Entrainment in Cavity Flows
Nobs-78396 The Linearized Theory for Supercavitating Hydrofoils Operating at High Speeds Near a Free Surface
No. 011-3 Dynamic Heaving Motion of Ground Effect Machines
No.001-16 The Design of Base-Vented Struts for High Speed Hydrofoil Systems
No. 115-4 On the Pulsation of Finite Ventilated Cavities
No. 001-10 (I) The Stability Derivatives of a Hydrofoil Boat-Part I
No. 001-10(II) The Stability Derivatives of Hydrofoil Boat-Part II

Box9

No. 127-4 Ventilation Inception
No. 119-7 Linearized Theory for a Supercavitating Hydrofoil Operating in a Fluid of Finite Depth
No.001-12 Downwash Due to a Fully Cavitated Hydrofoil Beneath a Free Surface
No. 119-5 Fully Cavitating Hydrofoils Non-Steady Motion Under a Free Surface
No. 001-13 Mathematical Generation of Realistic Sea
No. 001-15 Low-Drag Base Vented Hydrofoils Designed for Operation Near the Free Surface
No. 001-5 The Static Performance of an Aspect Ratio 2/3 Ground Effect Machine
No.343-1 Experimental Investigation of the 5-Inch Chord Model of the Buships Parent Supercavitating Hydrofoil
No. 463-1 Hydronautics , Incorporated
No.463-4 On a Fully Cavitating Two-Dimensional Flat Plate Hydrofoil with Non-Zero Cavitation Number Near a Free Surface
No.463-2 Non-Steady Hydrodynamic Characteristics of a Supercavitating Hydrofoil Under a Free Surface
No.463-5 On Fully -Cavitating Hydrofoils Entering Gusts Under a Free Surface
No. 463-3 The Linearized Theory for a Supercavitating Biplane Operating at Zero Cavitation Number Near a Free Surface
No. 011-6 The Static Performance of Ground Effect Machines with Aspect Ratios of 1/3 2/3 1-1/2 3
No. 343-2 Experimental Investigation of a Supercavitating Hydrofoil with upper Surface Spoiler Flaps

Box10

No. 463-6 Passive Load Alleviation on Supercavitating Hydrofoils
No. 507-1 The Static Performance of a Model of the Tail Foil For The Grumman 80 Knot Transit Foil System
No.507-3 Experimental Investigation of the 1/4 Scale Tail Foil Model of the 80 Knot Transit Foil System
No.503-1 Higher Order Wave Theory For Slender Ships
505-1 The Dynamic Pressure Trace at the Sea Bottom Created By a Ground Effect Machine
No. 605-2 Choking of Strut -Ventilated Foil Cavities
No.463-10 Hydrofoil Craft Dynamics in a Realistic Sea Including Automatic Control
No. 709-1 On the Flow Field Beneath a Moving Pressure Distribution Over the Sea
No.707-2 Cavitation Inception for a Two-Dimensional Half Body in a Uniform Stream with a Free Surface and a Solid Bottom
No. 711-1 On Cab Flaps In Non-Uniform Motion
No. 603-2 The Steady-State and Oscillatory Hydrodynamics of a 20^0 DeadRise Planing Surface
No. 809-1 Experimental Determination of the Static and Dynamic Coefficients of Surface-Piercing Struts

Box 11

No.S-2 National Advisory Committee for Aeronautics N.A.C.A. Tank CM2
No Yo-44 National Advisory Committee for Aeronautics N.A.C.A. Tank CM3
No.S-4 National Advisory Committee for Aeronautics N.A.C.A. Tank CM4
No.S-4 National Advisory Committee for Aeronautics N.A.C. A. Tank CM5
No.Yo-44 National Advisory Committee for Aeronautics N.A.C.A. Tank CM6
National Advisory Committee for Aeronautics N.A.C.A. Tank CM7
National Advisory Committee for Aeronautics N.A.C.A. Tank CM9
No.XA-942 National Advisory Committee for AeronauticsCM11
No. 38-3430 National Advisory Committee for Aeronautics CM 13
No. 37-15750 National Advisory Committee for Aeronautics CM 14
National Advisory Committee for Aeronautics CM15
No.HS-340 National Advisory Committee for Aeronautics CM 18
No. 49 National Advisory Committee for Aeronautics CM 19
No. 156 National Advisory Committee for Aeronautics CM 23
No. 314 National Advisory Committee for Aeronautics CM 24

Box12

No.XPB2Y-1 National Advisory Committee for Aeronautics CM 25
National Advisory Committee for Aeronautics CM 26
No. 160 National Advisory Committee for Aeronautics CM 27
National Advisory Committee for Aeronautics CM 28
No. 160 and 162 National Advisory Committee for Aeronautics CM 29
National Advisory Committee for Aeronautics CM 30
No. 77,78,79 National Advisory Committee for Aeronautics CM 31
No. 77,78,79 National Advisory Committee for Aeronautics CM 31-A
No. 77 National Advisory Committee for Aeronautics CM 33 Part I.
No. 78 National Advisory Committee for Aeronautics CM 33 Part.II.
No. 79 National Advisory Committee for Aeronautics CM 33 Part.III
No. 18 National Advisory Committee for Aeronautics CM 34
National Advisory Committee for Aeronautics CM 37
No. 59 National Advisory Committee for Aeronautics CM 38
National Advisory Committee for Aeronautics CM 39
National Advisory Committee for Aeronautics CM 40

Box 13

No.54 National Advisory Committee for Aeronautics CM 41
No.55 National Advisory Committee for Aeronautics CM 42
No.77-A National Advisory Committee for Aeronautics CM 43
No.79-A,79-B National Advisory Committee for Aeronautics CM 44
No. 77-F National Advisory Committee for Aeronautics CM 45
No. 78-B National Advisory Committee for Aeronautics CM 46
No.77-G,77-H,77-J, 77-K National Advisory Committee for Aeronautics CM 47
No.76-B,76-C, 76-C, 76-D, 76-E, 76-F National Advisory Committee for Aeronautics CM 52
National Advisory Committee for Aeronautics CM 48
No.87 National Advisory Committee for Aeronautics CM 49
National Advisory Committee for Aeronautics CM 53
No.86 National Advisory Committee for Aeronautics CM 54
No.95 National Advisory Committee for Aeronautics CM 55
No.94 National Advisory Committee for Aeronautics CM 57
No.95 National Advisory Committee for Aeronautics CM 59
No.96 National Advisory Committee for Aeronautics CM 62

Box 14

National Advisory Committee for Aeronautics CM 63
No.100 National Advisory Committee for Aeronautics CM 64
No.94-F National Advisory Committee for Aeronautics CM 66
No.102 National Advisory Committee for Aeronautics CM 67
National Advisory Committee for Aeronautics CM 68
No.106/107 National Advisory Committee for Aeronautics CM 73
No. 72-p National Advisory Committee for Aeronautics CM 74

Box 15

No.108 National Advisory Committee for Aeronautics CM 76
No.110 National Advisory Committee for Aeronautics CM 77
No.110-L National Advisory Committee for Aeronautics CM 78
No.110-M National Advisory Committee for Aeronautics CM 80
No.120 National Advisory Committee for Aeronautics CM 83
No.112 National Advisory Committee for Aeronautics CM 84
No.84 National Advisory Committee for Aeronautics CM 85

Box 16

No.L6F08 Ditching Tests of A 1/20 -Size Model of the Army B-32 Airplane in Langley Tank No.2
No.L6F26 Ditching Tests with A1/20 -Size Model of the Army B-29 Airplane Broken in Two Parts
No.L6G03 Ditching Tests with A 1/11-Size Model of the Navy PV-1 Airplane (Army B-34) in Langley Tank No.2
National Advisory Committee for Aeronautics MR-190
National Advisory Committee for Aeronautics MR-190
National Advisory Committee for Aeronautics MR-192
National Advisory Committee for Aeronautics MR-193
National Advisory Committee for Aeronautics MR-197
No.L6B04 Ditching Tests with 1/20 Size Models of the Army B-29 Airplane in Langley Tank No. 2 and From an Outdoor Catapult
No. L6B04 Ditching Tests with 1/20-Size Models of the Army B-29 Airplane in Langley Tank No. 2 and From an Outdoor Catapult
No.L6D24a Ditching Tests of a Model of the Army B-24 Airplane with Parachutes and Antenna Fairings
No. L6D23 Take-Off Tests of a Navy PBY2Y-3 Flying Boat with and without Jet Assistance
National Advisory Committee for Aeronautics MR 86
National Advisory Committee for Aeronautics MR 87
National Advisory Committee for Aeronautics MR 88
National Advisory Committee for Aeronautics MR 89
National Advisory Committee for Aeronautics MR 92

Box 17

No. 121 National Advisory Committee for Aeronautics MR 90
No. 83 National Advisory Committee for Aeronautics MR 91
No.116 National Advisory Committee for Aeronautics MR 93
No.124 National Advisory Committee for Aeronautics MR 94
No.104 National Advisory Committee for Aeronautics MR 95
No.116 National Advisory Committee for Aeronautics MR 96
No.124-D-1 National Advisory Committee for Aeronautics MR 97
No.120-R National Advisory Committee for Aeronautics MR 100

Box 18

No.124D-3 National Advisory Committee for Aeronautics MR 101
No.106-D to 106-M National Advisory Committee for Aeronautics MR 105
No.125 National Advisory Committee for Aeronautics MR 106
National Advisory Committee for Aeronautics MR 108
National Advisory Committee for Aeronautics MR 110
National Advisory Committee for Aeronautics MR 111
National Advisory Committee for Aeronautics MR 112
National Advisory Committee for Aeronautics MR 113
National Advisory Committee for Aeronautics MR 117
No.116 E-2 National Advisory Committee for Aeronautics MR 118
No. 139 National Advisory Committee for Aeronautics MR 119
No.133 National Advisory Committee for Aeronautics MR 120
No.140 National Advisory Committee for Aeronautics MR 121
No.141 National Advisory Committee for Aeronautics MR 122

Box 19

National Advisory Committee for Aeronautics MR124
National Advisory Committee for Aeronautics MR 123
No.67,67A,67B,67C National Advisory Committee for Aeronautics MR 125
National Advisory Committee for Aeronautics MR 128
No.155 National Advisory Committee for Aeronautics MR 127
National Advisory Committee for Aeronautics MR 129
No. 116E-3K, 120R, and 143 National Advisory Committee for Aeronautics MR 132
National Advisory Committee for Aeronautics MR 133
National Advisory Committee for Aeronautics MR 136
No.143 National Advisory Committee for Aeronautics MR 137
No.143 National Advisory Committee for Aeronautics MR 138
No.124 E National Advisory Committee for Aeronautics MR 141
No.157A and 157 B National Advisory committee for Aeronautics MR 143
No. 156, 156-A and 156 -B National Advisory Committee for Aeronautics MR 145
No.153C and 153 D National Advisory Committee for Aeronautics MR 150
No.131-X National Advisory Committee for Aeronautics MR 152
National Advisory Committee for Aeronautics MR 153
No.143E National Advisory Committee for Aeronautics MR 154
National Advisory Committee for Aeronautics MR 155
National Advisory Committee for Aeronautics MR 157
No.165B and 165C National Advisory Committee for Aeronautics MR-159

Box 20

No.132 National Advisory Committee for Aeronautics MR-160
No.164 J National Advisory Committee for Aeronautics MR-161
No.158 National Advisory Committee for Aeronautics MR -162
National Advisory Committee for Aeronautics MR-167
No.158-1 National Advisory Committee for Aeronautics MR-164
No.171 National Advisory Committee for Aeronautics MR-168
No.171 National Advisory Committee for Aeronautics MR-168
No. 195A, 195B,196A,196B National Advisory Committee for Aeronautics MR-169
No. 57-B-6 and 57-B-7 National Advisory Committee for Aeronautics MR-170
National Advisory Committee for Aeronautics MR-172
National Advisory Committee for Aeronautics MR-173
National Advisory Committee for Aeronautics MR-174
No.164 National Advisory Committee for Aeronautics MR-175
No.A-20A National Advisory Committee for Aeronautics MR-177
National Advisory Committee for Aeronautics MR-178
No.162 National Advisory Committee for Aeronautics MR-180
No.192 National Advisory Committee for Aeronautics MR-182
No.206 National Advisory Committee for Aeronautics MR-191
National Advisory Committee for Aeronautics MR-188

Box 21

July 1941 The Effect of External Shape upon the Drag of a Scoop
May 1940 Consideration of Auxiliary Jet Propulsion for Assisting Take-off
August 1941 Formulas for use in Boundary-Layer Calculations
August 1941 Wind-Tunnel Investigation of Control-Surface Characteristics II-A large Aerodynamic Balance of Various nose shapes with a 30-Percent-Chord Flap on an NACA 0009 Airfoil
December 1941 Tank Tests of a 1/5 Full-size Dynamically Similar Model of the Army OA-9 Amphibian with Motor-Driven Propellers -NACA Model 117
March 1942 The Aerodynamic Tests of Three EDO Floats for the SB2U -2, and XSB2C-2 Seaplanes -NACA Models 106-k,107-k, 125-AH
June 1942 The Effect of Pitch on Force and Moment Characteristics of Full-scale Propellers of five Solidities
July 1942 Wind-Tunnel of the Effects of Propeller Operation and Flap Deflection on the Pitching Moments and Elevator Hinge Moments of a Single-Engine Pursuit-Type Airplane
November 1942 Control-Motion Studies of the PBM-3 Flying Boat in Abrupt Pull-ups
January 1943 General Free to Trim Tests in NACA Tank No. 2 of Three 1/8 Full Size Models of Flying Boats Hulls at Low Speeds -NACA Models 116E-3k, 12oR, 143
January 1943 Investigation of the Effect of Spray Strips on the Low-Speed Spray Characteristics of a 1/8 -Size Model of the Consolidated PB2Y-3 Flying Boat -NACA Model 116E-3
January 1943 Stability and Control Tests of a 3/4 Scale Model of The XP-59 Airplane in the NACA Full-scale Tunnel
August 1941 Static Characteristic of Hamilton Standard Propellers Having Clark Y and NACA 16 - Series Blade Sections
November 1941 Flight Measurements of the Elevator Deflections used in Landings of Several Airplanes
February 1943 NACA Radio Ground-Speed System for Aircraft
April 1943 Flight Tests of a Glider Model Towed By Twin Parallel Towlines
June 1943 Preliminary Tank Tests with Planing -Tail Seaplane Hulls
June 1943 Tank Tests of a 1/8 Size Dynamic Model of the PB2Y-3 Airplane with Simulated Jet Motors - NACA Models 131J, 131J-1, 131J-2
June 1943 Tank Tests of a 1/8 Size Dynamic Model of the PB2Y-3 Airplane with increased power-NACA Model 131
April 1944 Preliminary Tank Tests of an Outboard Float Having the Form of a Streamline Body of Revolution Fitted with a Hydrofoil
April 1944 Spin-Tunnel Tests of a 1/57.33-Scale Model of the Northrop XB-35 Airplane
May and July 1944 Wind-Tunnel Investigation of a 1/20 Scale Powered Model of a Four-Engine Transport Airplane
August 1944 Ditching Tests with a 1/12 Size Model of the Army B-26 Airplane in NACA Tank No. 2 and on an Outdoor Catapult
June 1944 Resistance Tests of a 1/16 Size Model of the Hughes-Kaiser Flying Boat, NACA Model 183
July 1944 Wind-Tunnel Investigation of the Effect of Jet-Motor Operation on Stability

Box 22

September 1944 The Design of the Optimum Hull for a Large Long-range Flying Boat
September 1944 A Method for Predicting the Elevator Deflection Required to Land
October 1944 Dynamic Loads on Airplane Structures During Landing
October 1944 Ditching Tests with a 1/11 Size Model of the Army B-25 Airplane in NACA Tank No. 2 and on an Outdoor Catapult
July 1943 Wind-Tunnel of Four Full -Scale Seaplane Floats
September 1943 Aerodynamic and Hydrodynamic Tests of a Family of Models of Flying-Boat Hulls Derived From a Streamline Body NACA Model 84 Series
September 1943 Tests of a 1/40 Scale Wing-Hull and a 1/10 Scale Float-Strut Model of the Hughes Kaiser Cargo Airplane in the Two-dimensional Low-Turbulence Pressure Tunnel
October 1943 Analysis of Wind-Tunnel Stability And Control Tests in Terms of Flying Qualities of Full-scale Airplanes
October 1943 Effect of Length Beam Ratio on Resistance and Spray of Three Models of Flying Boat Hulls
November 1943 The Flow of a Compressible Fluid Past A Curved Surface
November 1943 Design Criterions for the Dimensions of the Forebody of a Long-range Flying Boat
November 1943 A Method for Making Quantitative Studies of the Main Spray Characteristics of Flying Boat Hull Models
December 1943 Some Systematic Model Experiments of the Bow-Spray Characteristics of Flying Boat Hulls Operating at Low Speeds in Waves
January 1944 Note on the Interpreration of Wake-Survey Data and its use in the Estimation of induced Drag Due to Irregularities
February 1944 Landing Characteristics of a Model of a Flying Boat with the Depth of Step Reduced to Zero By Means of a Retractable Planing Flap
February 1944 The Landing Stability of a Powered Dynamic Model of a Flying Boat with 30^0 V-Step and with two Depths of Transverse Step
March 1944 Measurements of Flying Qualities of Curtiss SB2C-1 Airplane
March 1944 Maximum Lift Coefficients of Airplanes Based on Sum of Wing and Tail Areas
November 1944 Frequency of Occurrence of Atmospheric Gusts and of Related Loads on Airplanes Structures
November 1944 Ditching Tests with a 1/10 Size Model of the Army A-20A Airplane in Langley Tank No. 2 and on an Outdoor Catapult
January 1945 The Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for theB-26 Airplane

Box 23

January 1945 Ditching Behavior of Military Airplanes as Effected by Ditching Aids
April 1945 Summary of Measurements in Langley Full Scale Tunnel of Maximum Lift Coefficients and Stalling Characteristics of Airplanes
April 1945 Tank Tests of a Flying Boat Model Equipped with Several Types of Fairing Designed to Reduced the Air Drag of the Main Step
April 1945 Spray Characteristics and Take-off and Landing Stability of Several Modifications of a 1/8 Size Model of the PBN-1 Flying Boat-NACA Model 192
April 1945 Ditching Tests with a 1/6 Size Dynamic Model of the Army B-24 Airplane in Langley Tank No. 2 And on an Outdoor Catapult
May 1945 Flight Tests of Dive-Recovery Flaps on an XP-51 Airplane
May 1945 Performance Selection Charts for Gliders and Twin Engine Tow Planes
June 1945 Performance of Compressor Turbine Jet Propulsion System
June 1945 Effects on Low-Speed Spray Characteristics Various Modifications to a Powered Model of the Boeing XPBB-1 Flying Boat
July 1945 The Effect of Some Design Parameters on Ditching Characteristics
July 1945 Tests of Four Full Scale Propellers to Determine The Effect of Trailing Edge Extensions on Propeller Aerodynamic Characteristics
July 1945 Theoretical and Experimental Dynamic Loads for a Prismatic Float Having and Angle of Dead Rise of 221/2
October 1945 Tank Tests of a Powered Dynamic of a Flying Boat Having an Afterbody Length Beam Ratio of 4.7 Langely Tank Model 203C-1
September 1945 Bibliography and Review of Information Relating to the Hydrodynamics of Seaplanes
September 1945 Resistance Tests of Models of Three Flying Boats Hulls with a Length Beam Ratio of 10.5
October 1945 The Resistance of Three Series of Flying Boat Hulls as Affected By Length Beam Ratio
January 1946 Spray Characteristics of a Powered Dynamic Model of a Flying Boat Having a Hull with a Length Beam Ratio 9.0
October 1945 The Effect of Afterbody Length of the Hydrodynamic Stability of a Dynamic Model of a Flying Boat Langley Tank Model 134
January 1946 Ditching Tests of a 1/8 Size Model of the Navy SB2C-1 Airplane (Army A-25) In Langley Tank No. 2 And on an Outdoor Catapult
June 1946 A Correlation of Loadings and Afterbody Length Beam Ratios of Various Flying Boat Hull
March 1943 Tests of a Dynamic Model in NACA Tank No. 1 To Determine The Effect of Length of Afterbody Angle of Afterbody Keel, Gross Loads, and a Pointed Step on Landing and Planing Stability
January 1946 Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16 Size Model
March 1946 Theory and Applications of Hot Wire Instruments in The Investigation of Turbulent Boundary Layers
March 1946 Approximate Formulas for the Computation of Turbulent Boundary Layer Momentum Thickness in Compressible Flows

Box 24

April 1946 Field of Flow About A Jet and Effect of Jets on Stability of Jet Propelled Airplanes
May 1946 Some Notes on the Effects of Jet Exit Design on Static Longitudinal Stability
June 1946 Parameters Determined Performance of Supersonic Pilotless Airplanes Powered By Ram-Compression Power Plants
No. 427 Seaplane Floats and Hulls Part I
No. 426 Seaplane Floats and Hulls Part II
No. 486 Tank Tests of Twin Seaplane Floats
No.622 Landing of Seaplanes
No. 676 Towing Tests of Models as an Aid in the Design of Seaplanes
No. 704 Scale Effect of Model in Seaplane Float Investigation
No. 719 Dimensions of Twin Seaplane Floats
No. 728 Aerodynamic Forces and Moments of A Seaplane on the Water
No.771 Ground Effect on the Take-off and Landing of Airplanes
No.863 On the Determination of the Take-off Characteristics of Seaplanes
No.1039 Pressure Distribution in Nonuniform Two Dimensional Flow
No. 1078 Experimental and Theoretical Investigation of Cavitation in water
No. 1247 Landing Procedure in Model Ditching Tests of Bf 109
No. 1256 The Boundary Layers in Fluids with Little Friction
No.1299 Additional Measurements of the Drag of Surface Irregularities in Turbulent Boundary Layers
No. 1335 Motion of a Cylinder Under the Surface of a Heavy Fluid
No.1345 Translational Motion of Bodies under the Surface of A Heavy Fluid of Finite Depth
No. 1359 Air-Water Analogy and the Study of Hydraulic Models

Box 25

No.350 Working Charts for the Selections of Aluminum Alloy Propellers of a Standard Form to Operate with Various Aircraft Engines and Bodies
No.365 Aerodynamic Characteristics of Circular-ARC AirFoils at High Speeds
No.372 The Gaseous Explosive Reaction-The Effect of Pressure on the Rate of Propagation of the Reaction Zone and Upon the Rate of Molecular Transformation
No.383 On the Theory of Wing Sections with Particular Reference to the Lift Distribution
No.405 Application of Practical Hydrodynamics to AirShip Design
No.450 The Calculation of Take-Off Run
No. 453 The Estimation of Maximum Load Capacity of Seaplanes and Flying Boats
No. 467 The Experimental Determination of The Moments of Inertia of Airplanes
No.481 Working Charts for the Determination of Propeller Thrust at Various Air Speeds
No.489 Air Conditions Close to the Ground and the Effect on Airplane Landings
No.497 Computation of the Two-Dimensional Flow in a Laminar Boundary Layer
No.503 The Effect of Spray Strips on the Take-Off Performance of a Model of a Flying Boat Hull
No.516 Potential Flow About Elongated Bodies of Revolution
No.527 Air Flow in a Separating Laminar Boundary Layer
No. 537 Tests in the Variable Density wind Tunnel of Related Airfoils Having the Maximum Camber Unusually Far Forward
No.540 Interference of Wing and Fuselage From Tests of 209 Combinations in the NACA Variable-Density Tunnel
No.543 Tank Tests of NACA Model 40 Series of Hulls for Small Flying Boats and Amphibians
No.558 Turbulence Factors of NACA Wind Tunnels as Determined by Sphere Tests
No.562 Air Flow in the Boundary Layer Near a Plate
No.581 Measurements of Intensity and Scale of Wind Tunnel Turbulence and Their Relations to the Critical Reynolds Number of Spheres
No. 625 A Discussion of Certain Problems Connected with the Design of Hulls of Flying Boats and the Use of General Tests DANA
No.626 The Transition Phase in the Take-Off of An Airplane
No.629 On Some Reciprocal Relations in the Theory of NonStationary Flows
No.631 Airfoil Section Characteristics as Applied to The Prediction of Air Forces and Their Distribution on Wings
No.642 Tests of Five Full Scale Propellers in the Presence of a Radial and Liquid Cooled Engine Nacelle, Including Tests of Two Spinners
No.702 The Calculated Effect of Various Hydrodynamic and Aerodynamic Factors on the Take-Off of a Large Flying Boat
No.753 Methods used in the NACA Tank for the Investigations of the Longitudinal Stability Characteristics of Models of Flying Boats
No.870 Tank Investigation of a Powered Dynamic Model of a Large Long-range Flying Boat
No.923 Effect of Afterbody Length and Keel Angle on Minimum Depth of Step for Landing Stability and on Take-off Stability of a Flying Boat
No. 1008 A Small Deflection Theory for Curved Sandwich Plates
No.1133 Mechanism of Start and Development of Aircraft Crash Fires
No.1135 Equations, Tables and Charts for Compressible Flow
No. 1195 Formulas for the Elastic Constants of Plates with Integral Waffle Like Stiffening
No.1204 Application of Several Methods for Determining Tansfer Functions and Frequency Response of Aircraft from Flight Data
No.1304 Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes
No.1347 Ditching Investigation of Dynamic Models and Effets of Design Parameters on Ditching Characteristics
May 1943 Characteristics of an NACA 66,S-209 Section Hydrofoil at Several Depths
April 1944 Wire-Strain Gage Hinge Moment Indicators for use in Tests of Airplane Models
March 1945 Comparison of Current Specifications with Actual Static Transverse Stability of 15 Flying Boats
October 1944 Possible Reduction in Air Drag Obtained By Retracting Wing-Tip Floats Compared with Reduction Obtained By Retracting Landing Gear

Box 26

NACA Instrumentation For Seaplane Tank Tests in Waves
February 1943 Investigation of the Effects of Ventilation on The Flow of Water Over a Rounded Chine
July 17 1943 The Use of Stubs for the Control of Bow Spray of a Flying Boat
Hydrodynamic Characteristics of an Aerodynamically Refined Planing-Tail Hull
Tank Tests of 1/5.5 Scale Powered Dynamic Model of the Columbia XJL-1 Amphibian Langley Tank Model 208 Tend No.NACA 2336
Tank Tests of a 1/7 Size Powered Dynamic Model of the Grumman XJR2F-1 Amphibian. Spray Characteristics Take Off and Landing Stability in Smooth Water-Langley Tank Model 212 Ted No.NACA 2378
Additional Abstracts Pertaining to Seaplanes
Ditching Tests of a 1/9 Size Model of the Army P-38 Airplane in Langley Tank No.2 And at the Outdoor Catapult
January 1947 Theoretical Analysis and Bench Tests of a Control Surface Booster Employing a Variable Displacement Hydraulic Pump
February 1947 Tank Tests of a 1/7 Size Dynamic Model of the Grumman XJR2F-1 Amphibian to Determine the Effect of Slotted and Split Type Flaps on Take Off Stability NACA Model 212 Ted.No. NACA 2378
Mar 10 1947 Ditching Tests of a 1/18 Scale Model of the Navy SP4M-1 Airplane in Langley Tank No. 2 and on an Outdoor Catapult Test No.NACA 2362
April 22, 1947 Correlation of the Trim Limits of Stability Obtained for a PB2Y-3 Flying Boat and a 1/8 Size Powered Dynamic Model
May 16 1947 Effect of Engine Skew on Directional and Lateral Control Characteristics of Single-Engine Airplanes
May 6 1947 Acceleration Measurements During Landing in Rough Water of a 1/7 Size Dynamic Model of Grumman XJR2F-1 Amphibian -Langley Tank Model 212 Ted No. NACA 2378
July 24 1947 Abstracts Pertaining To Seaplanes
November 26 1947 Preliminary Tank Tests of NACA Hydro-Skies for High Speeds Airplanes
December 9 1947 Tests of the Landing on Water of a Model of a High Speed Airplane Langley Tank Model 229
July 22 1948 Tank Spray Tests of a Jet Powered Model Fitted with NACA Hydo Skis
November 12 1948 Experimental Determination of the Lateral Stability of a Glider Towed by Single Towline and Correlation with an Approximate Theory
December 2 1948 Effects of a Sweptback Hydrofoil on the Force and Longitudinal Stabiliry Characteristics of a Typical High Speed Airplane
January 7 1949 The Effect of Air Jets Simulating Chines or Multiple Steps on the Hydrodynamic Characteristics of a Streamline Fuselage
February 11 1949 Aerodynamic Characteristics of a Flying-Boat Hull Having a Length Beam Ratio of 15 and a Warped Forebody
March 28 1949 Hydrodynamic Characteristics of Aerodynamically Refined Planning Tail Hulls
March 17 1949 The Effect of Rear Chine Strips on the Take-off Characteristics of a High Speed Airplane Fitted with NACA Hydro Skis
March 9 1949 Naval Research Laboratory , Department of the Navy Calibration Tests of a Japanese Log Rodmeter
March 17 1949 Naval Research Laboratory , Department of the Navy Calibration Tests of a German Log Rodmeter
June 3 1949 The Effect of Air Jet and Strip Modifications on the Hydrodynamic Characteristics of the Streamline Fuselage of a Transonic Airplane
August 9 1949 Civil Aeronautics Administaration Ditching Test of a 1/18 Scale Model of the Lockheed Constelitation Airplane with Speedpak Attached

Box 27

September 12 1949 Hydrodynamic Characteristics of a Swept Planing Tail Hull
September 12 1949 Preliminary Wind-Tunnel Investigation at High Subsonic Speeds of Planing Tail, Blended and Airfoil Forebody Swept Hulls
September 22 1949 Civil Aeronautics Administration Ditching Investigation of a 1/20 Scale Model of the Boeing Stratocruiser Airplane (C-97)
Dec 16 1949 Full Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425 Scale XP5M-1 Hull Bottom Ted No.NACA DE325
January 18 1950 Investigation of NACA 4-(0)(03)-045 and NACA 4-(0)(08)-045 Two Blade Propellers at Forward Mach Numbers To 0.925
February 21 1950 Hydrodynamic Force Characteristics of a Streamline Fuselage Modified by Either Breaker Strips or Rows of Air Jets Simulating Chines
April 20 1950 Ditching Tests of a 1/18 Scale Model of the Lockheed Constellation Airplane
May 18 1950 Ditching Tests with a 1/18 Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
May 4 1950 Model Ditching Investigation of the Douglas DC-4 and DC-6 Airplanes
June 12 1950 Tank Investigation of the Grumman JRF-5 Airplane Fitted with Hydro-Skis Suitable for Operation on water, Snow, And Ice
Oct 26 1950 Ditching Investigation of a 1/15 Scale Model of the Convair Liner Airplane
12-21-50 Tank Tests of an Alternate Hull form for the Consolidated Vultee PB2Y-3 Airplane
January 15 1951 An Investigation of the Hydrodynamic Characteristics of a Jet Powered Dynamic Model of the DR 56 Flying Boat Ted No., NACA DE 328
February 28 1951 An Investigation of the Spray Characteristics of a Jet Powered Dynamic Model of the DR 56 Flying Boat with a Vee Tail Ted No. NACA DE 328
Jul 10 1951 Compilation and Review of Effects of Design Parameters on Ditching Characteristics
August 7 1951 Tank Investigation of the Grumman JRF-5 Airplane with a Single Hydro-Skis and an Extended Afterbody
Sep 24 1951 Tank Investigation of the EDO Model 142 Hydro-Ski Research Airplane
November 7 1951 Hydrodynamic Investigation of a 1/13 Scale Model of The Consolidated Vultee Skate 7 Seaplane Equipped with Twin Hydro-Skis Ted No. NACA DE 342
January 10 1952 Hydrodynamic Directional Behavior of a Swept Planing Tail Hull
April 9 1952 Investigation of the Hydrodynamic Stability and Resistance of two Steamline Fuselages
April 10 1952 Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro Skis Ted No. NACA DE 357
February 24 1953 Experimental Investigation of The Flow Behind an Aspect Ratio 10 Hydrofoil Near the Water Surface
September 29 1953 Model Ditching Investigations of Three Airplanes Equipped with Hydro Skis
August 17 1954 An Investigation of the Hydrodynamic Characteristics of a 1/10 Size Powered Dynamic Model of the Martin M-267 Patrol Type Seaplane with Two Forebody Configuration
February 15 1955 An Aerodynamic and Hydrodynamic Investigation of Two Multi Jet Water Based Aircraft Having Low Transonic Drag Rise
July 6 1955 Reduction of Hydrodynamic Impact Loads for WaterBorne Aircraft
October 6 1955 Simulator Studies of a Simple Homing System
October 7 1955 A Comparison of the Hydrodynamic Forces on 1/25-1/10 and 8/10 Size Models of a Convair XF2Y-1 Hydro Ski
April 2 1956 Preliminary Measurements of the Aerodynamic Yawing Derivatives of a Triangular A Swept and an UnSwept Wing Performing Pure Yawing Oscillations with a Description of the Instrumentation Employed
May 17 1956 Full Scale Wind Tunnel Tests of the Longitudinal Stability and Control Characteristics of the XV-1 Convertiplane in the Autorotating Flight Range
October 31, 1956 Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading
March 20 1957 Investigation of the Influence of the Boundaries of a High-Speed Free Water Jet on the Planing Lift of a Flat Plate
March 27 1957 Statistical Approach to the Estimation of Loads and Pressure on Seaplane Hulls for Routine Operations
October 23 1957 Aerodynamic and Hydrodynamic Characteristics of a Proposed Supersonic MultiJet Based Hydro-Ski Aircraft with a Variable Incidence Wing

Box 28

March 1965 Theory and Operation of a Variable Exposure Photographic Pyrometer Over the Temperature Range 1800 -3600 F (1255-2255K)
March 1965 A Tension Shell Structure for Application to Entry Vehicles
1964 A Brief Study of Closed Circuit Television for Aircraft Landing
October 1966 Aerodynamic Center Considerations of Wings and Wing Body Combinations
August 1964 Force Test Investigation of a 1/4 Scale Model of The Modified VZ-2 Aircraft
January 1964 Characteristics of a Lunar Landing Configuration Having Various Multiple Leg Landing Gear Arrangements
October 1963 In Flight Shock Wave Pressure Measurements Above and Below A Bomber Airplane at Mach Numbers from 1.42-1.69
July 1963 Flight Test of a Pitch Control for Spinning Vehicle
1963 The Aerodynamic Design of Wings with Cambered Span Having Minimum Induced Drag
March 1965 Dynamic Model Investigation of the Landing Characteristics of a Manned Spacecraft
November 1960 Effect of Base Bleed and Terminal Fairings on the Performance of Exhaust Nozzle Afterbody Combinations at Mach Numbers of 1.93, 2.55 , 3.05
September 1960 Studies of the Retardation Force Developed on an Aircraft the Rolling in Slush or Water
March 1960 Ground Measurements of Airplane Shock-Wave Noise at Mach Numbers to 2.0 and at Altitudes to 60,000 Feet

Box 29

June 1960 The Supersonic Transport-A Technical Summary
February 1960 A Brief Investigation of a Hydro-Ski Stabilized Hydrofoil System on a Model of a Twin Engine Amphibian
May 1961 Skid Landings of Airplanes on Rocker Type Fuselages
May 1961 Calculated Normal Load Factors on Light Airplanes Traversing the Trailing Vortices of Heavy Transport Airplanes
June 1961 Large Scale Wind Tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps
August 1961 A Technique for Increasing the Sensitivity of a Solid State Fission Probe
March 1961 Review of Basic Principles of V/Stol Aerodynamics
A Study of Flutter at Low Mass Ratios with Possible Application to Hydrofoils
April 5, 1961 Draft for Sections on Vehicles Performance and Weather Capabilities
November 1962 Scanning Mechanism for a Satellite Borne X-Ray Spectrometer
September 1962 Simulator Studies of Simple Attitude Control for Spin -Stabilized Vehicles
April 1962 Receiving System Design for the Arraying of Independently Steerable Antennas for Deep Space Communications
December 1, 1959 Trajectory Control for Vehicles Entering the Earth's Atmosphere at Small Flight -Path Angles
December 1959 Model Investigations of Water Landings of a Winged Reentry Configuration Having Outboard Folding Wing Panels
October 1959 Water-Landing Impact Accelerations for Three Models of Reentry Capsules
October 1959 Rough Water Ditching Investigation of a Model of a Jet Transport with the Landing Gear Extended and With Various Ditching Aids
October 1962 VTOL Height-Control Requirements in Hovering as Determined from Motion Simulator Study

Box 30

No. 219 Experimental Towing Tank
No. 246 Experimental Towing Tank
No.247 Experimental Towing Tank
Feb.1946 No.299 A Rotating Arm for Towing Models of Ships and other Forms in Circular Paths
No. 254 Experimental Towing Tank
No. 167 On the Pressure Distribution for A Wedge Penetrating A Fluid Surface
No.169 The Discontinuous Fluid Flow Past An Immersed Wedge
Hydrodynamic Design of Seaplanes
Hydrodynamic Design of Seaplanes II
No. 57 Experimental Towing Tank
May 1948 No. 75 Underwater Photographs of Flow Patterns
July 1946 No.79 Review of Previously Published Rudder Studies
1955-1975 The Next 20 Years
1957 Three-dimensional Wave-Study Comes To Stevens
1957 A Study of The Hydrodynamic Impact Loads on a Dihedral Hydrofoil Suitable for Seaplane Use
June 1956 New Equipment for Model Tests at all Headings to Waves
June 1956 Measurements of Bending Moments on Models in Waves
June 1956 Planning for Three Dimensional Research in Waves
April 1953 New Open Water Propeller Testing Equipment and Initial Test Results

Box 31

No.155 Experimental Towing Tank
No.196 Experimental Towing Tank
July 1950 The Penetration of a Fluid Surface by a Wedge
No. 155 Porpoising Investigation on 1/30 Scale Model of XPB2M-1 Seaplane
No.196 Experimental Towing Tank
Received -July , 1950 The Penetration of a Fluid Surface

Box 32

No.732 October 1959 Longitudinal Stability of Surface-Piercing Hydrofoil Systems for Water -Based Aircraft
No.742 23 April 1959 A Model Investigation of the Low-Speed Roll and Yaw Characteristics of the P6M-2
No.70 Experimental Towing Tank
Quarterly Status Report for October, 1952 Research on Planing Surfaces

Box 33

September1, 1942 Model PBM-3 Hydrodynamic Report Engineering Report No. 1615
Water Loads Investigation Airplane Model XJR2F-1 Contract Noa (s)-4346 Report No. 2903.41
Water Loads Investigation Hull Bottom Pressures and Impact Loads ER 7516 November 1955 MARTIN
Water Loads Investigation Structural and Impact Loads Considering Airplane Flexibility ER 7515 November 1955 MARTIN
Proposal for Variable area Hydro-Ski Research and Development
Proposal for Anti-Submarine Warfare Airplane
No.831 Study of Change in Water Resistance Due to Change of Trim
The Design and Development of the Grumman Mallard by F.C. Rowley
No.5617TheHydrodynamic Design and Characteristics of A 20-Ton Hydrofoil Sea-Pallet
No.400 Proposal for the Analysis of Self-Excited Planing Vibration
No.5377 Proposal for a Hydrodynamic Study of Hull Forms Suitable for Large, High-Speed Hydrofoil Vessels

Box 34

Final Engineering Report Design and Installation of Grunberg Hydrofoil System on the JRF-5 Airplane
Final Engineering Report Instrumentation and Preliminary Flight Tests of the JRF-5 Equipped with a Grunberg Hydrofoil System
The Equilibrium Configuration of a Towed Hydrofoil-Cable System in Two-dimensional Steady Turns
Survey of Technical Information on Towed High-Speed Surface Vehicles
No. 590 The Equilibrium Configuration of a Towed Hydrofoil-Strut System in Two-dimensional Steady Turns
No. 5709 The Steady , Rectilinear Towing of Weightless Hydrofoil-Cable System in a Non-Uniform Stream

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NACA PHOTOS

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NACA PHOTOS