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- Test-Stand Investigation of Cooling Characteristics and Factors Affecting Temperature Distribution of a Double-Row Aircraft Engine
- Tests of a 1/7-Scale Powered Model of the Kaiser Tailless Airplane in the Langley Full-Scale Tunnel
- Tests of Cast Aluminum-Alloy Mixed-Flow Impellers
- The Influence of the Jet of a Propulsion Unit on Nearby Wings
- Investigation of Flow in a Centrifugal Pump
- Investigation of Turbulent Mixing Processes
- The Effect on the Sperry Directional Gyro in Turning
- Flight Measurements to Determine Effect of a Spring-Loaded Tab on Longitudinal Stability of an Airplane
- Flow Investigation With the Aid of the Ultramicroscope
- The Further Development of Heat-Resistant Materials for Aircraft Engines
- Investigations of Pressure Distribution on Fast Flying Bodies
- Correlation of Mixture Temperature Data Obtained From Bare Intake-Manifold Thermocouples
- The Effect of Liquid and Ice Particles on the Erosion of a Supercharger-Inlet Cover and Diffuser Vanes
- Efficiency of a Radial-Flow Exhaust-Gas Turbosupercharger Turbine With a 12.75-Inch Tip Diameter
- An Evaluation of the Knock-Limited Performance of Triptane
- Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients
- Annual Report of the National Advisory Committee for Aeronautics (28th). Administrative Report Including Technical Report Nos. 727 to 751
- The Effect of Increase in Combustion-Air Inlet Temperature From 80 to 130 F on the Sea-Level Performance of a 22-Inch-Diameter Pulse-Jet Engine
- Effects of Fuel-Vapor Loss on Knock-Limited Performance and Inspection Properties of Aviation Fuels
- The Effect of Ethylene Dibromide on the Knock-Limited Performance of Leaded and Nonleaded S Reference Fuel
- Determination of Towline Tension and Stability of Spin-Recovery Parachutes
- An Investigation of the Icing and Heated-Air De-Icing Characteristics of the R-2600-13 Induction System
- Performance of the Modified V-1710-93 Engine-Stage Supercharger with a Constant-Area Vaneless Diffuser
- Performance of the 19XB 10-Stage Axial-Flow Compressor
- Aerodynamic Characteristics of Several Modifications of a 0.45-Scale Model of the Vertical Tail of the Curtiss XP-62 Airplane
- Aerodynamic Data for a Wing Section of the Republic XF-12 Airplane Equipped With a Double Slotted Flap
- Aerodynamic Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor Blades
- Analysis of V-G Records from the SNB-1 Airplane
- Effect of Three Modifications on Performance of Auxiliary-Stage Supercharger for V-1710-93 Engine
- Free-Spinning-Tunnel Tests of a 1/18-Scale Model of the Fairchild XNQ-1 Airplane, TED No. NACA 2398
- Performance of 19XB-2A Gas Turbine 1 - Effect of Pressure Ratio and Inlet Pressure on Turbine Performance for an Inlet Temperature of 800 Degrees R
- Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 14S-T Aluminum Alloy
- Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-Type Airplane as Measured in Flight
- Altitude-Wind-Tunnel Investigation of Oil-System Performance of XR-4360-8 Engine in XTB2D-1 Airplane
- Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 4 - Curtiss 732-1C2-0 Four-Blade Propeller
- Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loading 2 - Curtiss 838-1C2-18R1 Four-Blade Propeller
- Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 6 - Hamilton Standard 6507A-2 Four- and Three-Blade Propellers
- Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 5 - Curtiss 836-14C2-18R1 Four-Blade Propeller
- Calibration Tunnel for High Speed
- Calibrations of Service Pitot Tubes in the Langley 24-Inch High-Speed Tunnel
- Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16-Size Model
- Airscrew Gyroscopic Moments
- An Investigation of Cowl-Flap and Cowl-Outlet Designs for the Boeing B-29 Power-Plant Installation
- Investigation of Ice Formation in the Induction System of an Aircraft Engine 1: Ground Tests
- Investigation of Ice Formation in the Induction System of an Aircraft Engine 2: Flight Tests
- An Investigation of Cowl Inlets for the B-29 Power-Plant Installation
- Flight Measurements by Various Methods of the Drag Characteristics of the XP-51 Airplane
- Flight Investigation to Improve the Dynamic Longitudinal Stability and Control-Feel Characteristics of the P-63A-1 Airplane (AAF No. 42-68889) with Closely Balanced Experimental Elevators
- Flight Investigation of Factors Affecting the Carburetor Ram and Nacelle Drag of an A-26B Airplane
- High-Speed Longitudinal-Stability and Control Characteristics of the Consolidated Vultee Lark Missile as Predicted from Wind-Tunnel Tests (TED No. NACA 2391)