Investigation of injectant properties on jet penetration in a supersonic stream
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6204
Reference17 articles.
1. Mean droplet size for cross-stream water injection into a Mach 8 airflow.
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