Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps

Author: Brown, Albert E
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56D03
Link: https://digital.library.unt.edu/ark:/67531/metadc62674/

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