Numerical computation of shock wave-turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill
By: S.-W. Kim.
Contributors: Institute for Computational Mechanics in Propulsion
Publisher: Lewis Research Center
Published: 1989
Place of publication: Cleveland, Ohio
Number of pages: 29
Subjects: Transonic flow; Turbulence models
Notes: Bibliographical references: p.23-26.