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Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds
Author:
Knapp, Ronald J
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53G14
Link:
https://digital.library.unt.edu/ark:/67531/metadc59667/
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