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Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)
Author:
Chauvin, Leo T.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57F27
Link:
https://digital.library.unt.edu/ark:/67531/metadc63788/
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