Numerical study of delta wing leading edge blowing /
by David Yeh, Domingo Tavella, and Leonard Roberts.

Description

Main Author: Yeh, David.
Related Names: Roberts, L.
Tavella, D. A.
Joint Institute for Aeronautics and Acoustics.
Language(s): English
Published: Stanford, CA : Stanford University, Department of Aeronautics and Astronautics, 1988.
Subjects: Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Mathematical models.
Vortex-motion > Vortex-motion / Mathematical models.
Lift (Aerodynamics) > Lift (Aerodynamics) / Mathematical models.
Leading edges (Aerodynamics) > Leading edges (Aerodynamics) / Mathematical models.
Note: At head of title: Joint Institute for Aeronautics and Acoustics.
"July 1988."
Cover title.
Physical Description: xv, 114 p. : ill. ; 28 cm.
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