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Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees
Author:
Lowry, John G
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3863
Link:
https://digital.library.unt.edu/ark:/67531/metadc56298/
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