Search U.S. government technical reports digitized or harvested by TRAIL.
An Experimental Investigation of Several Low-Drag Wing-Nacelle Combinations with Internal Air Flow
Cooling of Gas Turbines, 2, Effectiveness of Rim Cooling of Blades
Economy of internally cooling only the overheated cylinders of aircraft engines
General theory of airfoil sections having arbitrary shape or pressure distribution
In-line aircraft-engine bearing loads 2: blade-bearing loads
Improving engine cooling with special baffles
Method of Matching Performance of Compressor Systems with that of Aircraft Power Sections
Performance effect of fully shrouding a centrifugal supercharger impeller
A method for determining the rate of heat transfer from a wing or streamline body
A visual photographic study of cylinder lubrication
An investigation of backflow phenomenon in centrifugal compressors
Application of a numerical procedure to stress analysis of stringer-reinforced panels
The application of data on strength under repeated stresses to the design of aircraft
An Experimental Investigation of NACA Submerged-Duct Entrances
A general representation for axial-flow fans and turbines
The effect of two inlet-duct designs on turbine efficiency
An Experimental Investigation of NACA Submerged-Duct Entrances
Flight tests of a P-63-1 airplane with an electric torquemeter
Infrared-spectrophotometric analysis of binary and ternary mixtures of liquid hydrocarbons
Quantitative analysis for aromatic amines in aviation fuels by ultraviolet spectrophotometry