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- Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane
- Flight tests of various tail modifications on the Brewster XSBA-1 airplane I : measurements of flying qualities with original tail surfaces
- Full-scale tunnel tests of a flying model of the Curtiss XP-55 airplane
- Gasoline-water distribution coefficients of xylidines
- Free-spinning-tunnel tests of a model of a canard airplane
- Notes on maximum airplane angular velocities
- Effect of exhaust back pressure on engine power
- Determination of general relations for the behavior of turbulent boundary layers
- A method for studying piston friction
- Correlation of single-cylinder cooling tests of a Pratt and Whitney R-2800-21 engine cylinder with wind-tunnel tests of a Pratt and Whitney R-2800-27 engine
- A correlation of the dimensions, proportions, and loadings of existing seaplane floats and flying boat hulls
- Design criterions for the dimensions of the forebody of a long-range flying boat
- Effect of pH on strength of resin bonds
- Air-flow surveys in the region of the tail surfaces of a single-engine airplane equipped with dual-rotating propellers
- A comparative study of the effect of wing flutter shape on the critical flutter speed
- The belt method for measuring pressure distribution
- Effect of wing leading-edge slots on the spin and recovery characteristics of airplanes
- The significance of the time concept in engine detonation
- The effect of xylidines on the load-carrying capacity of an aircraft-engine oil I
- Effects of mean-line loading on the aerodynamic characteristics of some low-drag airfoils
- The effect of xylidines on the corrosiveness of aircraft-engine oil
- The effect of xylidines on the stability of an aircraft-engine lubricating oil
- The effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel
- The Heat Transfer to a Plate in Flow at High Speed
- Small-orifice tubes for minimizing dilution in exhaust-gas samples
- A flight investigation of fuselage static-pressure-vent airspeed installations
- General porpoising tests on flying-boat-hull models
- An investigation of aircraft heaters XI : measured and predicted performance of a slotted-fin exhaust gas and air heat exchanger
- An investigation of aircraft heaters XIII : performance of corrugated and noncorrugated fluted type exhaust gas-air heat exchangers
- An investigation of aircraft heaters XII : performance of a formed-plate crossflow exhaust gas and air heat exchanger
- The induction of water to the inlet air as a means of internal cooling in aircraft-engine cylinders
- XC-35 gust research project: Preliminary analysis of the lateral distribution of gust velocity along the span of an airplane
- Additional design charts relating to the stalling of tapered wings
- Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil
- The low-temperature solubility of technical xylidine in aviation gasoline
- Pressure loss in ducts with compound elbows
- Stability and control tests of a 3/4-scale model of the XP-69 airplane in the NACA full-scale tunnel
- High-speed wind-tunnel tests of a 1/14-scale model of a four-engine cargo airplane
- Development of thermal ice-prevention equipment for the B-24D airplane
- Development of thermal ice-prevention equipment for the B-17F airplane
- Elimination of rumble from the cooling ducts of a single-engine pursuit airplane
- Fatigue strength and related characteristics of spot-welded joints in 24S-T alclad sheet
- Flying qualities of a twin-engine patrol airplane as estimated from wind-tunnel tests
- A method for calculating heat transfer in the laminar flow region of bodies
- Observations of compressibility phenomena in flight
- Analysis of wind-tunnel stability and control tests in terms of flying qualities of full-scale airplanes
- Water tolerance of aviation gasoline containing xylidines
- Aerodynamic and hydrodynamic tests of a family of models of flying hulls derived from a streamline body -- NACA model 84 series
- Flight measurements of compressibility effects on a three-blade thin Clark Y propeller operating at constant advance-diameter ratio and blade angle
- Comparison of various methods for computing drag from wake surveys