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- On Wind Tunnel Tests and Computations Concerning the Problem of Shrouded Propellers
- On the Theory of the Laval Nozzle
- Exact Calculation of Laminar Boundary Layer in Longitudinal Flow Over a Flat Plate With Homogeneous Suction
- Experimental Flights for Testing of a Reactor as an Expedient for the Termination of Dangerous Spins
- Flow Measurement by Means of Light Interference
- Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane with Wing-Tip Tanks Installed
- Gas Motion in a Local Supersonic Region and Conditions of Potential-Flow Breakdown
- Heat Transmission in the Boundary Layer
- Jet Diffusion in Proximity of a Wall
- Lift Force of an Arrow-Shaped Wing
- Annual Report of the National Advisory Committee for Aeronautics (32nd). Administative Report Including Technical Report Nos. 834 to 862
- Annual Report of the National Advisory Committee for Aeronautics (30th). Administrative Report Including Technical Report Nos. 774 to 803
- Annual Report of the National Advisory Committee for Aeronautics (31st). Administrative Report Including Technical Report Nos. 804 to 833
- Computation of Thin-Walled Prismatic Shells
- The Effects of Horizontal-Tail Location and Wing Modifications on the High-Speed Stability and Control Characteristics of a 01.17-Scale Model of the McDonnell XF2H-1 Airplane (TED No, NACA DE336)
- Report on Investigation of Developed Turbulence
- Performance of Single-Stage Turbine of Mark 25 Torpedo Power Plant with Two Special Nozzles 1 - Efficiency with 0.45-inch Rotor Blades
- Preliminary Analysis of Axial-Flow Compressors Having Supersonic Velocity at the Entrance of the Stator
- General Characteristics of a Airspeed System using Fuselage Static Vents on a Swept-Wing Airplane
- Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the McDonnell XF2H-1 Airplane
- Performance of Axial-Flow Supersonic Compressor of XJ55-FF-1 Turbojet Engine 2 - Performance of Inlet Guide Vanes as Separate Component
- Comparison of Water-Load Distributions Obtained during Seaplane Landings with Bureau of Aeronautics Specifications. TED No. NACA 2413
- The Compressible Flow Past Various Plane Profiles Near Sonic Velocity
- Constant-Pressure Combustion Charts Including Effects of Diluent Addition
- Contribution to the Problem of Flow at High Speed
- Altitude Performance of AN-F-58 Fuels in British Rolls-Royce Nene Single Combustor
- Altitude-Test-Chamber Investigation of McDonnell Afterburner on J34 Engine
- Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom: TED No. NACA DE325
- High Speed Stability and Control Characteristics of a 0.17-Scale Model of the McDonnell XF2H-1 Airplane (TED No. NACA DE 318)
- Hydrodynamic Qualities of a 1/10-Size Powered Dynamic Model of the XP5Y-1 Flying Boat in Smooth Water: Langley Tank Model 246, TED No. NACA DE 320
- Longitudinal Characteristics of a Semispan Model of the Grumman Airplane Design 83 having a Sweptback Wing and of the Model with a Straight Wing as Determined from Wing-Flow Tests at Transonic Speeds, TED No. NACA DE337
- Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes with Tab Control: First Partial Report. Derivation of the Equations of Motion and their General Solutions
- Measurement of Oil-Film Pressures in Journal Bearings under Constant and Variable Loads
- Performance of Single-Stage Turbine of Mark 25 Torpedo Power Plant with Two Special Nozzles 3: Efficiency with Standard Rotor Blades
- On the Motions of an Oscillating System Under the Influence of Flip-Flop Controls
- On the Installation of Jet Engine Nacelles on a Wing Fourth Partial Report: Pressure-Distribution Measurements on a Sweptback Wing with Jet Engine Nacelle
- Two-Dimensional Compressible Flow in Turbomachines With Conic Flow Surfaces
- Two-Dimensional Wing Theory in the Supersonic Range
- Two-Dimensional Motion of a Gas at Large Supersonic Velocities
- Wind-Tunnel Tests on Various Types of Dive Brakes Mounted in Proximity of the Leading Edge of the Wing
- Test Report on Three- and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Trapezoidal Wing)
- Flow Pattern in a Converging-Diverging Nozzle
- Lame's Wave Functions of the Ellipsoid of Revolution
- Flight Investigation of 6.25-Inch-Diameter Deacon Rocket and 10-Inch-Scale Model Rocket
- Some New Problems on Shells and Thin Structures
- Spin and Recovery Characteristics of the Northrop XF-89 Airplane
- The Static-Pressure Error of a Wing Airspeed Installation of the McDonnell XF-88 Airplane in Dives to Transonic Speeds
- Investigation in Simulated Vertical Descent of the Characteristics of a Cargo-Dropping Device having Extensible Rotating Blades
- Investigation of a Systematic Group of NACA 1-Series Cowlings With and Without Spinners
- Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems