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SPC MD 54
by Webmaster - Sun 25 Jan 2026 01:18:PM
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#493484
Wed 27 Feb 2019 11:01:AM
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Joined: Feb 2001
Posts: 381,904
Launch Director
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OP
Launch Director
Joined: Feb 2001
Posts: 381,904 |
Abstract: An experimental campaign was conducted to measure and to characterize the freestream disturbance levels in the NASA Langley Research Center 20-Inch Mach 6 Wind Tunnel. A pitot rake was instrumented with fast pressure transducers, hot wires, and an atomic layer thermopile to quantify the fluctuation levels of pressure, mass flux, and heat flux, respectively. In conjunction with these probe-based measurements, focused laser differential interferometry was used to optically measure density fluct... Source: Measurements of Freestream Fluctuations in the NASA Langley 20-Inch Mach 6 Tunnel
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