Temperature measurements made in skin of wing, tested on model propelled by 2-stage rocket propulsion system, agreed well with calculated values; measured values of Stanton number were in reasonably good agreement with theory of Van Driest for flat plates with turbulent boundary layers.
Free-flight investigation of rocket-propelled model to determine aerodynamic heating on thin, unswept, untapered, multispar aluminum-alloy wing at mach numbers up to 2.22
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 12-15-58L
1959
38 pages
Report
Englisch
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