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Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36
Author:
Kaattari, George E.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A54J12
Link:
https://digital.library.unt.edu/ark:/67531/metadc60859/
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