Available Indexes

Numerical computation of shock wave :
turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill /
S.-W. Kim.

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Main Author: Kim, S.-W.
Language(s): English
Published: [Washington, DC] : National Aeronautics and Space Administration ; 1989]
Subjects: Boundary layer.
Aerodynamics, Transonic.
Note: Distributed to depository libraries in microfiche.
Physical Description: 30 p. 28 cm.
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Item Link Original Source
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