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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