Search U.S. government technical reports digitized or harvested by TRAIL.
Grain-Boundary Behavior in Creep of Aluminum Bicrystals
Ground-Simulator Study of the Effects of Stick Force and Displacement on Tracking Performance
Measurements of Turbulent Skin Friction on a Flat Plate at Transonic Speeds
Second Order Subsonic Airfoil-Section Theory and Its Practical Application
Investigation of Jet-Engine Noise Reduction by Screens Located Transversely Across the Jet
Effect of Oxygen Content of Furnace Atmosphere on Adherence of Vitreous Coatings to Iron
Total Lift and Pitching Moment on Thin Arrowhead Wings Oscillating in Supersonic Potential Flow
Contributions on the Mechanics of Boundary-Layer Transition
Influence of Shear Deformation of the Cross Section on Torsional Frequencies of Box Beams
Supplementary Charts for Estimating Performance of High-Performance Helicopters
Charts for Estimating Performance of High-Performance Helicopters
Theoretical Investigation of a Proportional-Plus-Flicker Automatic Pilot
An Approximate Solution for Axially Symmetric Flow Over a Cone With an Attached Shock Wave
Some Measurements of Time and Space Correlation in Wind Tunnel
Interaction of a Free Flame Front With a Turbulence Field
On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression
Optimum Flight Paths of Turbojet Aircraft
Steady Properly-Banked Turns of Turbojet-Propelled Airplanes
General Solutions of Optimum Problems in Nonstationary Flight
Incompressible Flutter Characteristics of Representative Aircraft Wings
Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure
Theory of Reversible and Nonreversible Cracks in Solids
Influence of Alloying upon Grain-Boundary Creep
Metallography of Aluminum and Its Alloys: Use of Electrolytic Polishing
Influence of Hot-Working Conditions on High-Temperature Properties of a Heat-Resistant Alloy
Contributions on the Mechanics of Boundary-Layer Transition
Charts for Estimating Performance of High-Performance Helicopters
Characteristics of Turbulence in Boundary Layer with Zero Pressure Gradient
Some Results of Flight Testing of Ski-Equipped Aircraft at the Naval Air Test Center
Study of Effects of Microstructure and Anisotropy on Fatigue of 23S-T4 Aluminum Alloy
Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips
Meteorological Problems Associated With Commercial Turbojet-Aircraft Operation