Three-dimensional computations of cross-flow injection and combustion in a supersonic flow
By: Mark H. Carpenter.
Contributors: American Institute of Aeronautics and Astronautics.
Publisher: American Institute of Aeronautics and Astronautics
Published: 1989
Place of publication: Washington, D. C
Number of pages: 16
Subjects: Combustion; Cross flow; Supersonic flow
Notes: Includes bibliographical references: p. 12.

Source: AIAA 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference Buffalo, N. Y/June 12-14, 1989