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- A Flight Investigation of Exhaust-Heat De-Icing, Special Report
- Investigation of the Boundary Layer About a Symmetrical Airfoil in a Wind Tunnel of Low Turbulence
- Flow Around Wings Accompanied by Separation of Vortices
- High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane
- Full-Scale Tests of 4- and 6-Blade, Single- and Dual-Rotating Propellers, Special Report
- Full-Scale Tests of Several Propellers Equipped with Spinners, Cuffs, Airfoil and Round Shanks, and NACA 16-Series Sections, Special Report
- Flight Tests of Exhaust-Gas Jet Propulsion
- Flight Tests of Exhaust Gas Jet Propulsion, Special Report
- Creep Strength of Stabilized Wrought-Aluminum Alloys
- Note on the Calculation of Boundary Layers
- Constant-Pressure Blowers
- Recent Work on Airfoil Theory
- High-speed drag tests of several fuselage shapes in combination with a wing
- A graphical method of determining pressure distribution in two-dimensional flow
- Stresses in Single-Spar Wing Constructions With Incompletely Built-Up Ribs
- Drag and propulsive characteristics of air-cooled engine-nacelle installations for two-engine airplanes
- Effect of body nose shape on the propulsive efficiency of a propeller
- Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel
- Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel, Special Report
- Investigation of the Characteristics of a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed Tunnel
- Wind tunnel tests of air inlet and outlet openings on a streamline body
- Propeller charts for the determination of the rotational speed for the maximum ratio of the propulsive efficiency to the specific fuel consumption
- Preliminary Tests in the NACA Tank to Investigate the Fundamental Characteristics of Hydrofoils
- Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap
- Wind-tunnel investigation of air inlet and outlet openings on a streamline body
- Annual Report of the National Advisory Committee for Aeronautics (25th). Administrative Report Including Technical Report Nos. 645 to 680
- Analysis of Wind-Tunnel Data on Directional Stability and Control
- The Calculated Effect of Various Hydrodynamic and Aerodynamic Factors on the Take-Off of a Large Flying Boat
- An Analysis of the Stability of an Airplane With Free Controls
- Flow coefficients of monosleeve valves
- Determination of ground effect from tests of a glider in towed flight
- Determination of the Characteristics of Tapered Wings
- A theoretical study of lateral stability with an automatic pilot
- A high-speed motion-picture study of normal combustion, knock and preignition in a spark-ignition engines
- Propeller analysis from experimental data
- Pressure distribution over NACA 23012 airfoil with a slotted and a split flap
- Piston temperatures in an air-cooled engine for various operating conditions
- Preliminary investigation of the flying qualities of airplanes
- Pressure available for cooling with cowling flaps
- The Aileron as an Aid to Recovery From the Spin
- Analysis of Cylinder-Pressure-Indicator Diagrams Showing Effects of Mixture Strength and Spark Timing
- Aerodynamic heating and the deflection of drops by an obstacle in an air stream in relation to aircraft icing
- Radiator design
- General Airfoil Theory
- Some comparative tests of plain and alclad 24S-T sheet
- Comparison of stress-strain curves obtained by single-thickness and pack methods
- Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with flight tests
- Compression tests of some 17S-T aluminum-alloy specimens of I cross section
- The effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression
- Effect of alternately high and low repeated stresses upon the fatigue strength of 25S-T aluminum alloy