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Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01
Author:
Lord, Douglas R.
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L58C07
Link:
https://digital.library.unt.edu/ark:/67531/metadc64060/
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