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Calculative method for estimating the interference pressure field at zero lift on a symmetrical swept-back wing mounted on a circular cylindrical body
Author:
Nielsen, Jack N.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A9E19
Link:
https://digital.library.unt.edu/ark:/67531/metadc58327/
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