An Experimental and Computational Investigation of Multiple Injection Ports in a Convergent-Divergent Nozzle for Fluidic Thrust Vectoring
Author:
Affiliation:
1. Analytical Services and Materials
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3802
Reference21 articles.
1. Future fighter technologies
2. Herrick, P. W.: Propulsion Influences on Air Combat. AIAA-85-1457,July1985.
3. Nguyen, L. T.; and Gilbert, W. P.: Impact of Emerging Technologies on Future Combat Aircraft Agility. AIAA-90-1304,May1990.
4. Herrick, P. W.: Air Combat Payoffs of Vectoring/Reversing Exhaust Nozzles. AIAA-88-3239,July1988.
5. Costes, P.: Investigation of Thrust Vectoring and Post-Stall Capability in Air Combat. AIAA-88-4160-CP,1988.
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