Search U.S. government technical reports digitized or harvested by TRAIL.
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
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 shear stress of a curved rectangular panel with a central stiffener
Biaxial fatigue strength of 24S-T aluminum alloy
Analysis of means of improving the uncontrolled lateral motions of personal airplanes
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
A study of flow changes associated with airfoil section drag rise at supercritical speeds
Dynamometer-stand investigation of a group of mufflers
Strength analysis of stiffened thick beam webs
Two-dimensional compressible flow in centrifugal compressors with straight blades
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
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
Design and calibration of a total-temperature probe for use at supersonic speeds
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