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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