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Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method
Author:
Emerson, Horace F.
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3671
Link:
https://digital.library.unt.edu/ark:/67531/metadc56768/
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