An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in an ionized argon flow
By: W. S. Liu.
Contributors: UTIAS
Series: UTIAS report -- no. 198
Publisher: Institute for Aerospace Studies
Published: 1975
Place of publication: [Downsview, Ont.]
Subjects: Argon; Laminar boundary layers; Nonequilibrium flow; Shock waves
Notes: Includes bibliographical references.