A low-speed investigation of a thin 60©� delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size

Author: Croom, Delwin R.
Year: 1955
Document Type: NACA
Issuing Agency: National Advisory Committee for Aeronautics,
SUDOC: Y 3.N21/5:15/L54L03a
Series: NACA research memorandum ;
Report Number: L54L03a
Subject: Delta wing airplanes--Aerodynamics--Testing
Link: https://hdl.handle.net/2027/mdp.39015086490425

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