Open ended shock tube flow as a tool to aid development of a two-dimensional compressible nonsteady computer code
By: E. G. Plett, M. B. Khalil and D. H. Gladstone.
Contributors: Gladstone, D. H.; Khalil, M. B.
Publisher: AIAA
Published: 1986
Place of publication: New York
Number of pages: 11
Subjects: Shock tubes
Notes: Bibliography: p.11.

Source: AIAA 24th Aerospace Sciences Meeting, Jan. 6-9, 1986