Check Calibration of the NASA Glenn 10- by 10-foot Supersonic Wind Tunnel (2014 Test Entry)
Title | Check Calibration of the NASA Glenn 10- by 10-foot Supersonic Wind Tunnel (2014 Test Entry) PDF eBook |
Author | Aaron Johnson |
Publisher | |
Pages | 15 |
Release | 2016 |
Genre | |
ISBN |
Calibration of the NASA Glenn Research Center 10-by 10-ft Supersonic Wind Tunnel (1993 and 1995 Tests)
Title | Calibration of the NASA Glenn Research Center 10-by 10-ft Supersonic Wind Tunnel (1993 and 1995 Tests) PDF eBook |
Author | |
Publisher | |
Pages | 42 |
Release | 2000 |
Genre | |
ISBN |
Subsonic Calibration of the NASA Glenn Research Center 10x10-foot Supersonic Wind Tunnel (1998 Tests)
Title | Subsonic Calibration of the NASA Glenn Research Center 10x10-foot Supersonic Wind Tunnel (1998 Tests) PDF eBook |
Author | E. Allen Arrington |
Publisher | |
Pages | |
Release | 2000 |
Genre | |
ISBN |
Calibration of the NASA Glenn 8- by 6-foot Supersonic Wind Tunnel (1996 and 1997 Tests)
Title | Calibration of the NASA Glenn 8- by 6-foot Supersonic Wind Tunnel (1996 and 1997 Tests) PDF eBook |
Author | E. Allen Arrington |
Publisher | |
Pages | 113 |
Release | 2012 |
Genre | |
ISBN |
Improved Pressure Measurement System for Calibration of the NASA LeRC 10x10 Supersonic Wind Tunnel
Title | Improved Pressure Measurement System for Calibration of the NASA LeRC 10x10 Supersonic Wind Tunnel PDF eBook |
Author | |
Publisher | |
Pages | 16 |
Release | 1994 |
Genre | |
ISBN |
NASA Glenn 1-by 1-Foot Supersonic Wind Tunnel User Manual
Title | NASA Glenn 1-by 1-Foot Supersonic Wind Tunnel User Manual PDF eBook |
Author | |
Publisher | |
Pages | 56 |
Release | 1999 |
Genre | |
ISBN |
NASA Glenn 1-By 1-Foot Supersonic Wind Tunnel User Manual
Title | NASA Glenn 1-By 1-Foot Supersonic Wind Tunnel User Manual PDF eBook |
Author | National Aeronautics and Space Adm Nasa |
Publisher | Independently Published |
Pages | 54 |
Release | 2018-09-20 |
Genre | Science |
ISBN | 9781723862748 |
This manual describes the NASA Glenn Research Center's 1 - by 1 -Foot Supersonic Wind Tunnel and provides information for customers who wish to conduct experiments in this facility. Tunnel performance envelopes of total pressure, total temperature, and dynamic pressure as a function of test section Mach number are presented. For each Mach number, maps are presented of Reynolds number per foot as a function of the total air temperature at the test section inlet for constant total air pressure at the inlet. General support systems-such as the service air, combustion air, altitude exhaust system, auxiliary bleed system, model hydraulic system, schlieren system, model pressure-sensitive paint, and laser sheet system are discussed. In addition, instrumentation and data processing, acquisition systems are described, pretest meeting formats and schedules are outlined, and customer responsibilities and personnel safety are addressed.Seablom, Kirk D. and Soeder, Ronald H. and Stark, David E. and Leone, John F. X. and Henry, Michael W.Glenn Research CenterMACH NUMBER; REYNOLDS NUMBER; SUPERSONIC WIND TUNNELS; SUPERSONIC FLOW; TEST CHAMBERS; DATA ACQUISITION; MANUALS; WIND TUNNEL NOZZLES; DYNAMIC PRESSURE; WIND TUNNEL TESTS