Approximate Analysis of Thrust Vector Control by Fluid Injection
Author:
Affiliation:
1. National Engineering Science Co., Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.5891
Reference8 articles.
1. Hausmann, G. F. "Thrust Axis Control of Supersonic Nozzles by Airjet Shock Interference/' United Aircraft Corp. Dept. Rep. R-63143-24, May 2, 1952.
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