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Flight-Determined Pressure Distributions Over the Wing of the Bell X-1 Research Airplane (10-Percent-Thick Wing) at Subsonic and Transonic Speeds
Author:
Knapp, Ronald J.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53D20
Link:
https://digital.library.unt.edu/ark:/67531/metadc59603/
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