The NASA Glenn Research Center's Hypersonic Tunnel Facility (HTF), located at the Plum Brook Station in Sandusky, Ohio, is a non-vitiated, free-jet facility, capable of testing large-scale propulsion systems at Mach Numbers from 5 to 7. As a result of a component failure in September of 1996, a restoration project was initiated in mid- 1997 to repair the damage to the facility. Following the 2-1/2 year effort, the HTF has been returned to an operational condition. Significant repairs and operational improvements have been implemented in order to ensure facility reliability and personnel safety. As of January 2000, this unique, state-of-the-art facility was ready for integrated systems testing
Described are the modifications currently under way to the Langley 8-Foot High Temperature Tunnel to...
A brief history of the 8x6 Supersonic Wind Tunnel (SWT) and 9x15 Low Speed Wind Tunnel (LSWT) at NAS...
NASA s HYPULSE facility at GASL has been reconfigured to permit free jet testing of the Hyper-X flow...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
A series of 15 integrated systems tests were conducted at the NASA Lewis Research Center's Hypersoni...
The Mach 10 Hyper-X ground test program is described, in which experimental flowpath parametric test...
The Hypervelocity Free-Flight Aerodynamic Facility, located at Ames Research Center, is NASA's only ...
A planned modification of the NASA Langley 8-Foot High Temperature Tunnel to make it a unique nation...
X3R is a new, large-scale free-piston driven reflected shock tunnel designed and operated at the Uni...
The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dr...
Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging ...
At hypersonic flight the kinetic energy of the flow is large enough that high temperature effects su...
Major upgrades were made in 1999 to the 6- by 9-Foot (1.8- by 2.7-m) Icing Research Tunnel (IRT) at ...
Research into hypersonic propulsion; i.e., supersonic combustion, was seriously initiated at the Lan...
Described are the modifications currently under way to the Langley 8-Foot High Temperature Tunnel to...
A brief history of the 8x6 Supersonic Wind Tunnel (SWT) and 9x15 Low Speed Wind Tunnel (LSWT) at NAS...
NASA s HYPULSE facility at GASL has been reconfigured to permit free jet testing of the Hyper-X flow...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
A series of 15 integrated systems tests were conducted at the NASA Lewis Research Center's Hypersoni...
The Mach 10 Hyper-X ground test program is described, in which experimental flowpath parametric test...
The Hypervelocity Free-Flight Aerodynamic Facility, located at Ames Research Center, is NASA's only ...
A planned modification of the NASA Langley 8-Foot High Temperature Tunnel to make it a unique nation...
X3R is a new, large-scale free-piston driven reflected shock tunnel designed and operated at the Uni...
The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dr...
Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging ...
At hypersonic flight the kinetic energy of the flow is large enough that high temperature effects su...
Major upgrades were made in 1999 to the 6- by 9-Foot (1.8- by 2.7-m) Icing Research Tunnel (IRT) at ...
Research into hypersonic propulsion; i.e., supersonic combustion, was seriously initiated at the Lan...
Described are the modifications currently under way to the Langley 8-Foot High Temperature Tunnel to...
A brief history of the 8x6 Supersonic Wind Tunnel (SWT) and 9x15 Low Speed Wind Tunnel (LSWT) at NAS...
NASA s HYPULSE facility at GASL has been reconfigured to permit free jet testing of the Hyper-X flow...