Numerical computation of shock wave
Subtitle: turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill
By: S.-W. Kim.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 101473; ICOMP -- 89-3
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1989
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Transonic.; Boundary layer.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 1 microfiche.