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Flight-determined pressure distributions over a section of the 35 degree swept wing of the Douglas D-558-II research airplane at Mach numbers up to 2.0
Author:
Jordan, Gareth H.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H55A03
Link:
https://digital.library.unt.edu/ark:/67531/metadc61081/
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