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- Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel
- Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage
- Aerodynamic Characteristics for Internal-Balance and Frise Type Ailerons on an NACA 6 Series Low-Drag Tip Section of the Wing for the XP-63 Airplane
- The Aerodynamic Tests of Three Edo Floats for the SB2U-3, 0S2U-2, and XSB2C-2 Seaplanes - NACA Models 106-K, 107-K, and 125-AH
- Aerodynamic Tests of an M-31 Bomb in the 8-Foot High-Speed Tunnel
- Self-Ignition and Combustion of Gases
- High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane
- High-Speed Wind-Tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-Scale Model
- Flight Measurements of the Aileron Characteristics of a Grumman F4F-3 Airplane
- Generalized equations for selection charts for heat exchangers in aircraft
- Generalized selection charts for bombers powered by one, two, four, and six 3000-horsepower engines 1: capacity and economy
- Generalized selection charts for bombers with four 2000-horsepower engines
- High-Speed Tests of a Ducted Body with Various Air-Outlet Openings
- Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines
- Shear-lag tests of two box beams with flat covers loaded to destruction
- Propeller Blade Stresses Caused by Periodic Displacement of the Propeller Shaft
- Correlation of Data on the Statistical Theory of Turbulence
- Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane
- Effect of airplane design efficiency and engine economy on range
- Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane
- Full-scale wind-tunnel and flight tests of a Fairchild XR2K-1 airplane with a zap flap and upper-surface aileron-wing installation
- The effect of dead rise upon the low-angle type of porpoising
- Effect of spring and gravity moments in the control system on the longitudinal stability of the Brewster XSBA-1 airplane
- Derivation of charts for determining the horizontal tail load variation with any elevator motion
- Tire friction coefficients and their relation to ground-run distance in landing
- Summary of V-G records taken on transport airplanes from 1932 to 1942
- Tests in the 19-foot pressure tunnel of a 1/2.75-scale model of the F4U-1 airplane with several balanced elevators, full-span flaps, and droppable gas tank
- A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls
- Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons
- Calculation of tab characteristics for flight conditions from wind-tunnel data
- Characteristics of plain and balanced elevators on a typical pursuit fuselage at attitudes simulating normal-flight and spin conditions
- The Characteristics of Two Model Six-Blade Counterrotating Pusher Propellers of Conventional and Improved Aerodynamic Design
- Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications
- Calibrations of pitot-static tubes at high speeds
- Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions
- Comparison of tightness of 78 degrees machine-countersunk rivets driven in holes prepared with 78 degrees and 82 degrees countersinking tools
- Condensation trails: Where they occur and what can be done about them
- The longitudinal stability of flying boats as determined by tests of models in the NACA tank 1: methods used for the investigation of longitudinal stability characteristics
- Effect of inlet-air velocity distribution on the metering pressure of an injection-type aircraft carburetor
- Exhaust-stack nozzle area and shape for individual cylinder exhaust-gas jet-propulsion system
- Wind-tunnel tests of single- and dual-rotating tractor propellers of large blade width
- Wind-tunnel investigation of an NACA full-span high-lift lateral-control combination 1: section characteristics, NACA 23012 airfoil
- Wind-tunnel investigation of control-surface characteristics 5: the use of a beveled trailing edge to reduce the hinge moment of a control surface
- Wind-tunnel investigation of control-surface characteristics 8: a large aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil
- A flight investigation of short-period longitudinal oscillations of an airplane with free elevator
- Flight investigation of the performance and cooling characteristics of a long-nose high-inlet-velocity cowling on the XP-42 airplane
- Flight investigation of an NACA ice-detector suitable for use as a rate-of-icing indicator
- A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap
- An Experimental Investigation of Flow Across Tube Banks
- An Investigation of Hydrofoils in the NACA Tank 1: Effect of Dihedral and Depth of Submersion