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- An Investigation of Ejection Releases of Submerged and Semisubmerged Dynamically Scaled Stores From a Simulated Bomb Bay of a Fighter-Bomber Airplane at Supersonic Speeds
- Investigation of Ejection Release Characteristics of Four Dynamically Scaled Internal-Store Shapes From a 1/17-Scale Simulated Bomb Bay of the Republic F-105 Airplane at Mach Numbers of 1.39 and 1.98
- Tabulated Pressure Data for a Series of Controls on a 60 Degree Delta Wing at Mach Numbers of 1.61 and 2.01
- Investigation of Afterburner Combustion Screech and Methods of Its Control at High Combustor Pressure Levels
- Attenuation of Tangential-Pressure Oscillations in a Liquid-Oxygen-n-Heptane Rocket Engine With Longitudinal Fins
- Simulated Flight Investigation of Scaled-Speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip
- Some Design and Operational Considerations of a Liquid-Hydrogen Fuel and Heat-Sink System for Turbojet-Engine Tests
- Some Interference Effects That Influence Vertical-Tail Loads at Supersonic Speeds
- Static Lateral-Directional Stability Characteristics of Five Contemporary Airplane Models From Wind-Tunnel Tests at High Subsonic and Supersonic Speeds
- Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
- Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages
- A Summary of Results Obtained During Flight Simulation of Several Aircraft Prototypes With Variable-Stability Airplanes
- Summary of Subsonic-Diffuser Data
- Full-Scale Wind-Tunnel Tests of a North American FJ-3 Airplane with a Spoiler-Slot-Deflector Lateral Control System
- Flight Test of a Solid-Fuel Ramjet With the Internal Surface of the Combustor Air Cooled
- Flutter Tests of a 1/25-Scale Model of the B-36J/RF-84F Tip-Coupled Airplane Configuration in the Langley 19-Foot Pressure Tunnel
- Investigation of a 1/22-Scale of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Static Longitudinal Stability and Control and Performance Characteristics at Transonic Speeds
- Annual Report of the National Advisory Committee for Aeronautics (42nd): Administrative Report without Technical Reports
- Aerodynamic Principles for the Design of Jet-Engine Induction Systems
- Aerodynamics of Missiles Employing Wings of Very Low Aspect Ratio
- Free-flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Deg Sweptback Wing of Aspect Ratio 4
- Turbine Failure Investigation of J65-W-4 Turbojet Engine in an Altitude Test Chamber
- An Analytic Study of Turbojet Engine Thrust Augmentation With Liquid Hydrogen, Pentaborane, Magnesium Slurry, and JP-4 Afterburner Fuels and a 220-Second Impulse Rocket
- Chemical and Physical Properties of a Boron-Carbon-Hydrogen Fuel Z-244 (NACA 55Z8)
- A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift
- Spontaneous Ignition Studies Relating to Lubricants of Reduced Flammability
- Design Criteria for Axisymmetric and Two-Dimensional Supersonic Inlets and Exits
- Correlation of Crippling Strength of Plate Structures With Material Properties
- Correlation of Supersonic Convective Heat-Transfer Coefficients From Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
- Boundary-Layer Growth and Shock Attenuation in a Shock Tube With Roughness
- Investigation of Suction Slot Shapes for Controlling a Turbulent Boundary Layer
- Investigation of the Effect of Impact Damage on Fatigue Strength of Jet-Engine Compressor Rotor Blades
- Investigation of Far Noise Field of Jets 2: Comparison of Air Jets and Jet Engines
- Investigation of the Use of the Thermal Decomposition of Nitrous Oxide to Produce Hypersonic Flow of a Gas Closely Resembling Air
- Tabulated Pressure Coefficient Data from a Tail Loads Investigation on a 1/15-Scale Model of the Goodyear XZP5K Airship
- Preliminary Internal Performance Data for a Variable-Ejector Assembly on the XJ79-GE-1 Turbojet Engine 1: Nonafterburning Configurations
- On Landing Gear Stresses
- Static Longitudinal Stability Characteristics of a Series of 90-Millimeter Artillery Shells at Mach Numbers of 0.8, 0.9, 1.0, and 1.2
- Wind-Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Degree Swept-Wing Airplane
- On the Theory of Thin Shallow Shells
- On the Calculation of Shallow Shells
- On the Theory of Anisotropic Shallow Shells
- Annual Report of the National Advisory Committee for Aeronautics (40th). Administrative Report Including Technical Report Nos. 1158-1209
- Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104A Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. AF-245
- Component Performance Investigation of J71 Experimental Turbine 2 - Internal-Flow Conditions with 97-Percent-Design Stator Areas
- Component Performance Investigation of J71 Experimental Turbine 4 - Effect of First-Stator Adjustment; Over-All Performance of J71-97 Turbine With 132-Percent-Design Stator Area
- Component Performance Investigation of J71 Experimental Turbine 3 - Effect of Third-Stage Shrouding on Over-All Performance
- Aeroelastic Problems of Airplane Design
- Altitude Acceleration Investigation of the RA-14 Avon Turbojet Engine
- Flight Investigation to Determine the Effect of Jet Exhaust on Drag, Trim Characteristics, and Afterbody Pressures of a 0.125-Scale Rocket Model of the McDonnell F-101A Airplane