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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