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The zero-lift drag of a 60 degree delta-wing-body combination (AGARD model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7
Author:
Piland, Robert O
Year:
1954
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3081
Link:
https://digital.library.unt.edu/ark:/67531/metadc56898/
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