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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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