Flow separation ahead of blunt bodies at supersonic speeds /

Flow separation ahead of blunt bodies at supersonic speeds / W. E. Moeckel.

Supersonic flow against blunt bodies placed in boundary layers is discussed, and it is concluded that wedge-shaped or conical dead-air regions should form ahead of the body for some ranges of body thickness. Analysis of this type of flow indicates that a maximum body thickness exists (relative to in...

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Bibliographic Details
Main Author: Moeckel, W. E. (Wolfgang E.)
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2418.
Subjects:
Air flow.
Aerodynamics, Supersonic.
Cone > Aerodynamics.
Wedges > Aerodynamics.
Boundary layer.

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Call Number: Y 3.N 21/5:6/2418
Y 3.N 21/5:6/2418 Available Place a Hold

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