Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model

Strass, H Kurt Stephens, Emily W
naca-rm-l57f06
August 06, 1957


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l57f06.pdf