Search U.S. government technical reports digitized or harvested by TRAIL.
Investigation of torsion creep-to-rupture properties of N-155 alloy
Investigation of off-design performance of shock-in-rotor type supersonic blading
The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions
Over-all performance of J35-A-23 two-stage turbine
The preparation, physical properties, and heats of combustion of four alkylsilanes
Low-speed characteristics of a wing having 63 degrees sweepback and uniform camber
Measurements of downwash and sidewash behind cruciform triangular wings at Mach number 1.4
Flame velocities of four alkylsilanes
Effect of spark repetition rate on the ignition limits of a single tubular combustor
Notes on low-lift buffeting and wing dropping at Mach numbers near 1
Determination of ram-jet combustion-chamber temperatures by means of total-pressure surveys
Criterions for prediction and control of ram-jet flow pulsations
Analytical investigation of ram-jet-engine performance in flight Mach number range from 3 to 7
Ceramic coatings for prevention of carbon absorption in four heat-resistant alloys
Combustion properties of aluminum as ram-jet fuel
Aerodynamic characteristics of wings designed for structural improvement