Publication Date:
2019-07-13
Description:
Nozzle wall hypersonic turbulent boundary layers at free stream Mach number, using pitot, hot wire, wall pressure fluctuation and static pressure measurements
Keywords:
FLUID MECHANICS
Type:
AIAA PAPER 70-746
,
FLUID AND PLASMA DYNAMICS CONFERENCE; Jun 29, 1970 - Jul 01, 1970; LOS ANGELES, CA|; TROPHYSICAL JOURNAL
Format:
text
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