Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46, by Frank J. Centolanzi et al.

Title:	Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46
Author:	Centolanzi, Frank J.
Author:	Ames Research Center
Note:	National Aeronautics and Space Administration, 1959

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Subject:	Aircraft control
Subject:	Aircraft stability
Subject:	Angle of attack
Subject:	Backwash
Subject:	Delta wings
Subject:	Downwash
Subject:	Dynamic pressure
Subject:	Flow distribution
Subject:	Mach number
Subject:	Performance prediction
Subject:	Rectangular wings
Subject:	Reynolds number
Subject:	Supersonic speed
Subject:	Trailing edges
Subject:	Wakes
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