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- Tank tests of three models of flying-boat hulls of the pointed-step type with different angles of dead rise - NACA model 35 series
- The Transport of Vorticity Through Fluids in Turbulent Motion: In the Light of the Prandtl and Taylor Theories
- The Question of Spontaneous Wing Oscillations: Determination of Critical Velocity Through Flight-Oscillation Tests
- Relative Efficiencies and Design Charts for Various Engine-Propeller Combinations, Special Report
- Analysis of the Three Lowest Bending Frequencies of a Rotating Propeller
- General Considerations on the Flow of Compressible Fluids
- Experimental Studies of the Effective Width of Buckled Sheets
- Tests for the Determination of the Stress Condition in Tension Fields
- Annual Report of the National Advisory Committee for Aeronautics (21st). Administrative Report Including Technical Report Nos. 508 to 541
- The quiescent-chamber type compression-ignition engine
- A simplified application of the method of operators to the calculation of disturbed motions of an airplane
- Turbulence factors of NACA wind tunnels as determined by sphere tests
- Calculated and measured pressure distributions over the midspan section of the NACA 4412 airfoil
- The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data
- Effect of nozzle design on fuel spray and flame formation in a high-speed compression-ignition engine
- Wing-nacelle-propeller interference for wings of various spans force and pressure-distribution tests
- Propulsion of a flapping and oscillating airfoil
- Span load distribution for tapered wings with partial-span flaps
- Pressure-distribution measurements on O-2H airplane in flight
- A study of the two-control operation of an airplane
- Prechamber compression-ignition engine performance
- Measurements of fuel distribution within sprays for fuel-injection engines
- Full-scale wind-tunnel to determine a satisfactory location for a service Pitot-static tube on a low-wing monoplane
- Combustion-engine temperatures by the sodium line-reversal method
- A Comparison of Corrosion-Resistant Steel (18 Percent Chromium - 8 Percent Nickel) and Aluminum Alloy (24st)
- Procedure for determining speed and climbing performance of airships
- Remarks on the Elastic Axis of Shell Wings
- Tank Tests of a Model of the NC Flying-Boat Hull - N.A.C.A. Model 44
- Tank tests of models of floats for single-float seaplanes - First series
- Performance of Air-Cooled Engine Cylinders Using Blower Cooling
- Boosted Performance of a Compression-Ignition Engine With a Displaced Piston
- Calculated Effect of Various Types of Flap on Take-Off Over Obstacles
- Tests of N.A.C.A. airfoils in the variable-density wind tunnel. Series 230
- A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y
- Effect of changes in tail arrangement upon the spinning of a low-wing monoplane model
- Friction of compression-ignition engines
- Tanks test of a model of the hull of the Navy PB-1 flying boat - N.A.C.A. Model 52
- Tank tests of models of flying boat hulls having longitudinal steps
- Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with a Fowler flap
- Carbon-monoxide indicators for aircraft
- Charts for Calculating the Performance of Airplanes Having Constant-Speed Propellers
- Estimation of moments of inertia of airplanes from design data
- Analysis and Model Tests of Autogiro Jump Take-Off
- Piloting technique for recovery from spins
- Notes on the technique of landing airplanes equipped with wing flaps
- Circular Motion of Bodies of Revolution
- The Performance of a DePalma Roots-Type Supercharger
- A study of autogiro rotor-blade oscillations in the plane of the rotor disk
- A general tank test of a model of the hull of the British Singapore IIC flying boat
- Wind-Tunnel Tests of Wing Flaps Suitable for Direct Control of Glide-Path Angle