skip to content
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
Author:
Strass, H. Kurt
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57F06
Link:
https://digital.library.unt.edu/ark:/67531/metadc63538/
< New search