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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
Document ID
19930089753
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strass, H Kurt
Stephens, Emily W
Date Acquired
August 16, 2013
Publication Date
August 6, 1957
Report/Patent Number
NACA-RM-L57F06
Report Number: NACA-RM-L57F06
Accession Number
93R19043
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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