Add to ORKGThe NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Aerodynamics, stability and control, propulsion, and environmental factors of the supersonic cruise ...
The results are presented for the Douglas Aircraft Company system studies related to high speed civi...
Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a n...
Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a n...
Flight constraints and aerodynamic characteristics of hypersonic research aircraf
Four hypersonic research airplane configurations found to be the most cost effective were selected f...
The fabrication of the various components of the HRE AIM was completed. The purge system necessary f...
Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will...
The conclusion evolved from the three phased study on the configuration development of the X-24C Hyp...
The goals of the NASA Hypersonic Research Engine (HRE) Project, which began in 1964, were to design,...
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
The Hypersonic Research Engine-Aerothermodynamic Integration Model (HRE-AIM) was designed, fabricate...
Instrumentation developments are reported for thrust measurement, gas sampling, temperature measurem...
Aerodynamic effects on rocket and launch vehicle design, shock tunnel simulation, jet exhaust flow, ...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Aerodynamics, stability and control, propulsion, and environmental factors of the supersonic cruise ...
The results are presented for the Douglas Aircraft Company system studies related to high speed civi...
Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a n...
Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a n...
Flight constraints and aerodynamic characteristics of hypersonic research aircraf
Four hypersonic research airplane configurations found to be the most cost effective were selected f...
The fabrication of the various components of the HRE AIM was completed. The purge system necessary f...
Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will...
The conclusion evolved from the three phased study on the configuration development of the X-24C Hyp...
The goals of the NASA Hypersonic Research Engine (HRE) Project, which began in 1964, were to design,...
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
The Hypersonic Research Engine-Aerothermodynamic Integration Model (HRE-AIM) was designed, fabricate...
Instrumentation developments are reported for thrust measurement, gas sampling, temperature measurem...
Aerodynamic effects on rocket and launch vehicle design, shock tunnel simulation, jet exhaust flow, ...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Aerodynamics, stability and control, propulsion, and environmental factors of the supersonic cruise ...
The results are presented for the Douglas Aircraft Company system studies related to high speed civi...