Search U.S. government technical reports digitized or harvested by TRAIL.
Deformation Analysis of Wing Structures
A Flight Investigation of the Thermal Performance of an Air-Heated Propeller
Empirical Method for Frequency Compensation of the Hot-Wire Anemometer
The Formation and Stability of Normal Shock Waves in Channel Flows
Some Considerations of the Lateral Stability of High-Speed Aircraft
Meteorological Conditions Associated With Flight Measurements of Atmospheric Turbulence
Foaming Volume and Foam Stability
A Review of Boundary-Layer Literature
Marine Exposure Tests on Stainless Steel Sheet
Correlation of Two Experimental Methods of Determining the Rolling Characteristics of Unswept Wings
Effect of Slipstream Rotation in Producing Asymmetric Forces on a Fuselage
An Investigation of the Effect of Blade Curvature on Centrifugal-Impeller Performance
The Preparation and Physical Properties of Several Aliphatic Hydrocarbons and Intermediates
Bending Stresses Due to Torsion in a Tapered Box Beam
Effect of Aerodynamic Refinement on the Aerodynamic Characteristics of a Flying-Boat Hull
Device for Measuring Principal Curvature and Principal Strains on a Nearly Plane Surface
Wind-Tunnel Investigation of Icing of an Engine Cooling-Fan Installation
Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 75S-T Sheet
A Metallurgical Investigation of Large Forged Discs of Low-Carbon N-155 Alloy
A Study of Piston-Ring Friction
Effect of Geometric Dihedral on the Aerodynamic Characteristics of Two Isolated Vee-Tail Surfaces
The Spot Welding of Dissimilar Aluminum Alloys in the 0.040-Inch Thickness
The Spot Welding of Alclad 24S-T in Thicknesses of 0.064, 0.081, and 0.102 Inch
Flight Investigation of Thrust Augmentation of a Turbojet Engine by Water-Alcohol Injection
Estimation of Range of Stability Derivatives for Current and Future Pilotless Aircraft
A Device for Measuring Sonic Velocity and Compressor Mach Number
Tests of Submerged Duct Installation on a Modified Airplane in the Ames 40- by 80-foot Wind Tunnel
Estimate of Hull-Weight Change with Varying Length-Beam Ratio for Flying Boats