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- On the Problems of Chaplygin for Mixed Sub-and Supersonic Flows
- Pressure Distribution Measurements on a Turbine Rotor Blade Passing Behind a Turbine Nozzle Lattice
- Rockets Using Liquid Oxygen
- Rocket Power Plants Based on Nitric Acid and their Specific Propulsive Weights
- Report on Rocket Power Plants Based on T-Substance
- The Monoplane as a Lifting Vortex Surface
- The Oscillating Circular Airfoil on the Basis of Potential Theory
- The Turbulent Flow in Diffusers of Small Divergence Angle
- Wind-Tunnel Investigations on a Changed Mustang Profile with Nose Flap Force and Pressure-Distribution Measurements
- Theory of Wings in Nonstationary Flow
- Three-Component Force and Mass-Flow Measurement on a Jet Nacelle
- Tunnel Correction for Compressible Subsonic Flow
- Test Report on Three-and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Elliptic Wing)
- Abstracts Pertaining to Seaplanes
- Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212: TED No. NACA 2378
- Aerodynamic Characteristics at High Speeds of Full-Scale Propellers Having Different Shank Designs
- The Flow Through Axial Turbine Stages of Large Radial Blade Length
- Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 3: Control of Jet Engines
- Fundamental Aerodynamic Investigations for Development of Arrow-Stabilized Projectiles
- Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 2: Principles of Control Common to Jet, Turbine-Propeller Jet, and Ducted-Fan Jet Power Plants
- Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 1: Standardization of the Computations Relating to the Control of Gas-Turbine Power Plants for Aircraft by the Employment of the Laws of Similarity
- The Lift Distribution of Swept-Back Wings
- Laboratory Report on the Investigation of the Flow Around Two Turbine-Blade Profiles Using the Interferometer Method
- Lift Increase by Blowing Out Air, Tests on Airfoil of 12 Percent Thickness, Using Various Types of Flap
- Effects of Induction-System Icing on Aircraft-Engine Operating Characteristics
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 12, 1947 to July 18, 1947 at Clinton County Army Air Field, Ohio
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 24, 1946 to August 6, 1946 at Orlando, Florida
- Investigation of Single-Stage Modified Turbine of Mark 25 Torpedo Power Plant
- An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel Part 5 - Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage TED No. NACA DE308, Part V, Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage, TED No. NACA DE308
- Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane (Army No. 44-85099) - Stalling Characteristics
- Free-Spinning Tunnel Tests of a 1/24-Scale Model of the Grumman XTB3F-1 Airplane, TED No. NACA DE304
- Aerodynamic Characteristics of a Portion of the Horizontal Tail from a Douglas C-74 Airplane with Fabric-Covered Elevators
- Aerodynamic Characteristics of Three Deep-Stepped Planing-Tail Flying-Boat Hulls
- Ditching Tests with a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
- Spin and Recovery Characteristics of the Curtiss-Wright XP-87 Airplane
- Supplementary Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the McDonnell XB-85 Airplane Equipped with a Conventional-Tail Arrangement
- Supplementary Data on Airspeeds and Mach Numbers Attained by Lockheed Constellation Airplanes in Transcontinental Operations
- Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift
- Tests of Submerged Duct Installation on the Ryan FR-1 Airplane in the Ames 40- by 80-Foot Wind Tunnel
- Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (The Efficiency of Shock Diffusers)
- Free-Spinning-Tunnel Tests of a 1/27-Scale Model of the Douglas XF3D-1 Airplane, TED No. NACA DE 312
- High-Speed Wind-Tunnel Tests of a Model of the Lockheed YP-80A Airplane Including Correlation with Flight Tests and Tests of Dive-Recovery Flaps
- Gas-Dynamic Investigations of the Pulse-Jet Tube, Parts 1 and 2
- General Characteristics of the Flow through Nozzles at Near Critical Speeds
- Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane (Army No. 44-85099): Longitudinal-Stability and -Control Characteristics
- Force Tests of a 1/5-Scale Model of the McDonnell XP-85 Airplane with Conventional Tail Assembly in the Langley Free-Flight Tunnel
- Investigation of 10-Stage Axial-Flow X24C-2 Compressor, 1, Performance at Inlet Pressure of 21 Inches Mercury Absolute and Inlet Temperature of 538 Degrees R
- Performance of Compressor of XJ-41-V Turbojet Engine 2 - Static-Pressure Ratios and Limitation of Maximum Flow at Equivalent Compressor Speed of 8000 RPM
- Investigations on Experimental Impellers for Axial Blowers
- The Elasto-Plastic Stability of Plates