Search U.S. government technical reports digitized or harvested by TRAIL.
The Photoviscous Properties of Fluids
The Electrical Structure of Thunderstorms
The Formation of Ice on Aircraft
Cooling in Cruising Flight With Low Fuel-Air Ratios
Drag and Propulsive Characteristics of Air-Cooled Engine-Nacelle Installations for Large Airplane
The Effect of Cowling Shape on the Stability Characteristics of an Airplane
Recent Results in Rocket Flight Technique
Cooling Tests of an Air-Cooled Engine Cylinder With Copper Fins on the Barrel
Contribution to the Design of Plywood Shells
A Brief Study of the Speed Reduction of Overtaking Airplanes by Means of Air Brakes
Generalized Selection Charts for Harrison and Tubular Intercoolers
The Performance of a Vaneless Diffuser Fan
The Navier-Stokes Stress Principle for Viscous Fluids
Two-Dimensional Potential Flow Past an Ordinary Thick Wing Profile
Wind-Tunnel Investigations of Diving Brakes
Theory of Heat Transfer in Smooth and Rough Pipes
Application of Balancing Tabs to Ailerons
Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage
Aerodynamic Tests of an M-31 Bomb in the 8-Foot High-Speed Tunnel
Self-Ignition and Combustion of Gases
High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane
High-Speed Wind-Tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-Scale Model
Flight Measurements of the Aileron Characteristics of a Grumman F4F-3 Airplane
Generalized equations for selection charts for heat exchangers in aircraft
Generalized selection charts for bombers with four 2000-horsepower engines
High-Speed Tests of a Ducted Body with Various Air-Outlet Openings
Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines
Shear-lag tests of two box beams with flat covers loaded to destruction
Propeller Blade Stresses Caused by Periodic Displacement of the Propeller Shaft
Correlation of Data on the Statistical Theory of Turbulence
Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane
Effect of airplane design efficiency and engine economy on range
Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane