论文信息 - Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20 - 字舞流文

Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20

Nozzle wall hypersonic turbulent boundary layers at free stream Mach number, using pitot, hot wire, wall pressure fluctuation and static pressure measurements

D. V. Maddalon | L. Weinstein | R. Wagner | M. Fischer

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