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Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Author:
Keener, Earl R.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H55G07
Link:
https://digital.library.unt.edu/ark:/67531/metadc61544/
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