Search U.S. government technical reports digitized or harvested by TRAIL.
Chordwise and Spanwise Loadings Measured at Low Speed on Large Triangular Wings
Design Factors for 4- by 8-Inch Ram-Jet Combustor
Calculation of Aerodynamic Forces on a Propeller in Pitch or Yaw
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle
Measurements of Aileron Effectiveness of Bell X-1 Airplane Up to a Mach Number of 0.82
Measurements of Aileron Effectiveness of the Bell X-1 Airplane at Mach Numbers Between 0.9 and 1.06
Investigation of a Two-Step Nozzle in an 11-Inch Hypersonic Tunnel
Flight Investigation of the Jettisonable-Nose Method of Pilot Escape Using Rocket-Propelled Models
Flight Investigation of Flutter Models With 1/10-Scale Douglas D-558-2 Wing Panels
Hydrodynamic Characteristics of Aerodynamically Refined Planing-Tail Hulls
Rotation in Free Fall of Rectangular Wings of Elongated Shape