Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6
By: J. P. Vermeulen and G. Simeonides.
Contributors: Simeonides, G.; von Karman Institute for Fluid Dynamics
Series: von Karman Institute for Fluid Dynamics. Technical note -- 181
Publisher: von Karman Institute for Fluid Dynamics
Published: 1992
Place of publication: Rhode Saint Genese, Belgium
Number of pages: 75
Subjects: Hypersonic vehicles; Shock-boundary layer interaction
Notes: Includes bibliographical references: p. 43-46.