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- Further experiments on the flow and heat transfer in a heated turbulent air jet
- On the flying qualities of helicopters
- Determination of plate compressive strengths at elevated temperatures
- Effect of forebody warp and increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio
- Corrosion tests of a heated wing utilizing an exhaust-gas-air mixture for ice prevention
- Critical shear stress of infinitely long, simply supported plate with transverse stiffeners
- Critical axial-compressive stress of a curved rectangular panel with a central longitudinal stiffener
- Critical shear stress of a curved rectangular panel with a central stiffener
- Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow
- Determination of centrifugal-compressor performance on basis of static-pressure measurements in vaneless diffuser
- Biaxial fatigue strength of 24S-T aluminum alloy
- Comparison between predicted and observed performance of gas-turbine stator blade designed for free-vortex flow
- Analysis of means of improving the uncontrolled lateral motions of personal airplanes
- Annular-jet ejectors
- Compressive buckling of flat rectangular metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges
- Compressive buckling of simply supported plates with longitudinal stiffeners
- Boundary-layer and stalling characteristics of the NACA 64A006 airfoil section
- Effect of various compounds in use with airplane engines upon foaming of aircraft lubricating oil
- Effect of forebody warp on the hydrodynamic qualities of a hypothetical flying boat having a hull length-beam ratio of 15
- Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speed
- A study of flow changes associated with airfoil section drag rise at supercritical speeds
- Study by the Prandtl-Glauert method of compressibility effects and critical Mach number for ellipsoids of various aspect ratios and thickness ratios
- Dynamometer-stand investigation of a group of mufflers
- An investigation of aircraft heaters XXXI : summary of laboratory testing of several exhaust-gas and air heat exchangers
- Strength analysis of stiffened thick beam webs
- Triangular wings cambered and twisted to support specified distributions of lift at supersonic speeds
- Two-dimensional compressible flow in centrifugal compressors with straight blades
- Two-dimensional investigation of five related NACA airfoil sections designed for rotating-wing aircraft
- Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound
- Two matrix methods for calculating forcing functions from known responses
- Linear theory of boundary effects in open wind tunnels with finite jet lengths
- Linearized compressible-flow theory for sonic flight speeds
- Investigations relating to the extension of laminar flow by means of boundary-layer suction through slots
- Plastic buckling of simply supported compressed plates
- Plastic buckling of extruded composite sections in compression
- The influence of blade-width distribution on propeller characteristics
- Effect of hull length-beam ratio on the hydrodynamic characteristics of flying boats in waves
- An introduction to the physical aspects of helicopter stability
- Plastic buckling of a long flat plate under combined shear and longitudinal compression
- Stresses in and general instability of monocoque cylinders with cutouts VIII : calculation of the buckling load of cylinders with long symmetric cutout subjected to pure bending
- Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies
- Wind-tunnel investigation of the opening characteristics, drag, and stability of several hemispherical parachutes
- Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment
- Comparison of the structural efficiency of panels having straight-web and curved-web Y-section stiffeners
- Design and calibration of a total-temperature probe for use at supersonic speeds
- Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels with Longitudinal Extruded Z-Section Stiffeners
- Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels Having Small, Thin, Widely Spaced, Longitudinal Extruded Z-Section Stiffeners
- The application of airfoil studies to helicopter rotor design
- Boundary-layer and stalling characteristics of the NACA 63-009 airfoil section
- An analysis of the effect of lift-drag ratio and stalling speed on landing-flare characteristics