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High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane-dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1
Author:
Robinson, Harold L.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8H05
Link:
https://digital.library.unt.edu/ark:/67531/metadc57949/
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