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A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock
Author:
Harrin, Eziaslav N
Year:
1952
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2765
Link:
https://digital.library.unt.edu/ark:/67531/metadc56463/
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