Search U.S. government technical reports digitized or harvested by TRAIL.
Investigation of a High-Flow Transonic-Compressor Inlet Stage Having a Hub-Tip Radius of 0.35
Fatigue Behavior of Aircraft Structural Beams
Relationship of Metal Surfaces to Heat-Aging Properties of Adhesive Bonds
Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil
Accelerations in Transport-Airplane Crashes
Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04
Experimental techniques for predicting store motions during release or ejection
Some Research on the Lift and Stability of Wing-Body Combinations
Boundary-Layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6