Add to ORKGA series of 15 integrated systems tests were conducted at the NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) with test conditions simulating flight up to Mach 6. Facility stagnation conditions up to 3050 R and 1050 psia were obtained with typical test times of 20 to 45 sec
New hypervelocity capabilities for scramjet testing have recently been demonstrated in the HYPULSE S...
As true with all hypersonic flight, the ability to quickly and accurately predict the aero-thermodyn...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
The Mach 10 Hyper-X ground test program is described, in which experimental flowpath parametric test...
The NASA Langley 8-Foot High Temperature Tunnel has recently been modified to produce a unique testi...
The NASA Langley 8-Foot High Temperature Tunnel has recently been modified to produce a unique testi...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
This report presents results of gas analyses of Mach 7 Tunnel Calibration Test 139 conducted in the ...
Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging ...
The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dr...
Tests of the Hyper-X scramjet engine flowpath have been conducted in the HYPULSE shock tunnel at con...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
The high speed flows with mach number above 5 are generally categorised as hypersonic flows. In orde...
Airframe-integrated scramjet engine tests have 8 completed at Mach 7 in the NASA Langley 8-Foot High...
New hypervelocity capabilities for scramjet testing have recently been demonstrated in the HYPULSE S...
As true with all hypersonic flight, the ability to quickly and accurately predict the aero-thermodyn...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion...
The Mach 10 Hyper-X ground test program is described, in which experimental flowpath parametric test...
The NASA Langley 8-Foot High Temperature Tunnel has recently been modified to produce a unique testi...
The NASA Langley 8-Foot High Temperature Tunnel has recently been modified to produce a unique testi...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
This report presents results of gas analyses of Mach 7 Tunnel Calibration Test 139 conducted in the ...
Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging ...
The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dr...
Tests of the Hyper-X scramjet engine flowpath have been conducted in the HYPULSE shock tunnel at con...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
The high speed flows with mach number above 5 are generally categorised as hypersonic flows. In orde...
Airframe-integrated scramjet engine tests have 8 completed at Mach 7 in the NASA Langley 8-Foot High...
New hypervelocity capabilities for scramjet testing have recently been demonstrated in the HYPULSE S...
As true with all hypersonic flight, the ability to quickly and accurately predict the aero-thermodyn...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...