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Subsonic Mach and Reynolds number effects on the surface pressures, gap flow, pressure recovery, and drag of a nonrotating NACA 1-series E-type cowling at an angle of attack of 0 degrees
Author:
Reynolds, Robert M
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A51E03
Link:
https://digital.library.unt.edu/ark:/67531/metadc58878/
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