An experimental research program conducted to expand the operational capabilities of the NASA Langley Mach 7 Scramjet Test Facility is described. Previous scramjet testing in this facility was limited to a single simulated flight condition of Mach 6.9 at an altitude of 115,300 ft. The arc heater research demonstrates the potential of the facility for scramjet testing at simulated flight conditions from Mach 4 (at altitudes from 77,000 to 114,000 ft) to Mach 7 (at latitudes from 108,000 to 149,000 ft). Arc heater electrical characteristics, operational problems, measurements of nitrogen oxide contaminants, and total-temperature profiles are discussed
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
Proposed configurations for the next generation of transatmospheric vehicles will rely on air breath...
High enthalpy arc tunnel at Langley Research Center for simulating aerodynamic heating and forces du...
Operating characteristics of the Langley Mach 7 Scramjet Test Facility are described. The facility i...
A planned modification of the NASA Langley 8-Foot High Temperature Tunnel to make it a unique nation...
An engine test facility was constructed at the NASA Langley Research Center in support of a superson...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
This study reviews facility capabilities of NASA, Ames Research Center to simulate hypersonic flight...
Research programs at the NASA Langley Research Center on the development of airframe-integrated scra...
Reports by the staff of the University of Queensland on various research studies related to the adva...
This work represents an initial attempt to determine what, if any, issues arise from scaling demonst...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
Hypersonic missiles re-entering the atmosphere are subjected to severe aerodynamic heating. In order...
The Hypersonic Materials Environmental Test System (HyMETS) arc-jet facility located at the NASA Lan...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
Proposed configurations for the next generation of transatmospheric vehicles will rely on air breath...
High enthalpy arc tunnel at Langley Research Center for simulating aerodynamic heating and forces du...
Operating characteristics of the Langley Mach 7 Scramjet Test Facility are described. The facility i...
A planned modification of the NASA Langley 8-Foot High Temperature Tunnel to make it a unique nation...
An engine test facility was constructed at the NASA Langley Research Center in support of a superson...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
This study reviews facility capabilities of NASA, Ames Research Center to simulate hypersonic flight...
Research programs at the NASA Langley Research Center on the development of airframe-integrated scra...
Reports by the staff of the University of Queensland on various research studies related to the adva...
This work represents an initial attempt to determine what, if any, issues arise from scaling demonst...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
Hypersonic missiles re-entering the atmosphere are subjected to severe aerodynamic heating. In order...
The Hypersonic Materials Environmental Test System (HyMETS) arc-jet facility located at the NASA Lan...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
Proposed configurations for the next generation of transatmospheric vehicles will rely on air breath...
High enthalpy arc tunnel at Langley Research Center for simulating aerodynamic heating and forces du...