Investigation of effectiveness of a wing equipped with a 50-percent-chord sliding flap, a 30-percent-chord slotted flap, and a 30-percent-chord slat in deflecting propeller slipstreams downward for vertical take-off

Author: Kuhn, Richard E
Year: 1957
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3919
Link: https://digital.library.unt.edu/ark:/67531/metadc56598/

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