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Experimental investigation of the flow around lifting symmetrical double-wedge airfoils at Mach numbers of 1.30 and 1.41
Author:
Gooderum, Paul B.
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3626
Link:
https://digital.library.unt.edu/ark:/67531/metadc57890/
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