Search U.S. government technical reports digitized or harvested by TRAIL.
Heat-transfer tests of a steel cylinder barrel with aluminum fins of optimum proportions
Drag analysis of single-engine military airplanes tested in the NACA full-scale wind tunnel
The design of cooling ducts with special reference to the boundary layer at the inlet
Effect of wing loading, aspect ratio, and span loading of flight performances
Estimation of critical speeds of airfoils and streamline bodies
The problem of cooling an air-cooled cylinder on an aircraft engine
Longitudinal stability and control with special reference to slipstream effects
Design charts relating to the stalling of tapered wings
Aerodynamic characteristics of horizontal tail surfaces
The unsteady lift of a wing of finite aspect ratio
Measured Moments of Inertia of 32 Airplanes
Propeller Rotation Noise Due to Torque and Thrust
Measurement of the Forces Acting on Gliders in Towed Flight
A Full-Scale Investigation of the Effect of Several Factors on the Shimmy of Cantering Wheels
The Flow of a Compressible Fluid Past a Sphere
Ionization in the Knock Zone of an Internal-Combustion Engine
A Generalized Vortex Theory of the Screw Propeller and Its Application
The Development of Electrical Strain Gages
Factors Affecting Heat Transfer in the Internal-Combustion Engine
Structural Tests of a Stainless Steel Wing Panel by Hydrostatic Loading
Mathematical Analysis of Aircraft Intercooler Design
Extension of Pack Method for Compressive Tests
A Simple Approximation Method for Obtaining the Spanwise Lift Distribution
The Torsion of Box Beams With One Side Lacking
Measurement of Knock Characteristics in Spark-Ignition Engines
The Lead Susceptibility of Fuels and Its Dependence on the Chemical Composition
Pressure and Temperature Measurement in Supercharger Investigations
Experimental Contribution to the Study of Combustion in Compression-Ignition Engines
Experiments on Ball and Roller Bearings Under Conditions of High Speed and Small Oil Supply
Buckling Tests With a Spar-Rib Grill
Corrections on the Thermometer Reading in an Air Stream
The Shock-Absorbed System of the Airplane Landing Gear
Standards for Discharge Measurement With Standardized Nozzles and Orifices
Tests of Lead-Bronze Bearings in the DVL Bearing-Testing Machine
Testing of High-Octane Fuels in the Single-Cylinder Airplane Engine
Italian High-Speed Airplane Engines
Limits of Single-Stage Compression in Centrifugal Superchargers for Aircraft
Experimental Results With Airfoils Tested in the High-Speed Tunnel at Guidonia
General Relationships Between the Various Systems of Reference Axes Employed in Flight Mechanics
The Cause of Welding Cracks in Aircraft Steels
Theoretical and Experimental Investigations of the Drag of Installed Aircraft Radiators