A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection
By: N. D. Domel and D. S. Thompson.
Contributors: Thompson, D. S.; AIAA
Publisher: American Institute of Aeronautics and Astronautics
Published: 1991
Place of publication: Washington, D. C
Number of pages: 11
Subjects: Mixing; Supersonic combustion
Notes: Includes bibliographical references; p. 6.

Source: 29th Aerospace Sciences Meeting, Reno, Nevada, january 7-10, 1991