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Transonic Flight Tests to Determine Zero-Lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
Author:
Hoffman, Sherwood
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51K02
Link:
https://digital.library.unt.edu/ark:/67531/metadc58984/
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