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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