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- Strength Investigations in Aircraft Construction Under Repeated Application of the Load
- Progress Report on Strength and Creep of Special Ceramic Bodies in Tension at Elevated Temperatures
- Some Notes on the Effects of Jet-Exit Design on Static Longitudinal Stability
- Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 6 Degrees and 9 Degrees Trim and a 22-1/2 Degree Angle of Dead Rise
- Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 12 Degree Trim and With a 22-1/2 Degree Angle of Dead Rise
- Wind-Tunnel Investigation of Control-Surface Characteristics of Plain and Balanced Flaps on an NACA 0009 Elliptical Semispan Wing
- Wind-Tunnel Tests to Determine Aileron Characteristics of the McDonnell XFD-1 Airplane, TED No. NACA 23102
- A Correlation of the Effects of Compression Ratio and Inlet-Air Temperature on the Knock Limits of Aviation Fuels in a CFR Engine 2
- Kinetics of Chemical Reactions in Flames
- Wind-Tunnel Tests and Analysis of Three 10-Foot-Diameter Three-Blade Tractor Propellers Differing in Pitch Distribution
- Tests of the Jet-Motor Air-Intake Duct System on a 1/4-Scale Stub-Wing Model of a Pursuit-Type Airplane
- 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