Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference38 articles.
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2. Waithe, K. A.: An Experimental and Computational Investigation of Multiple Injection Ports in a Convergent-Divergent Nozzle for Fluidic Thrust Vectoring. MasterofScienceThesis,May2001.
3. Wing, David J.; and Giuliano, V. J.: Fluidic Thrust Vectoring of an Axisymmetric Exhaust Nozzle at Static Conditions. ASMEFEDSM97-3228,June1997.
4. Giuliano, V. J.; and Wing, D. J.: StaticInvestigation of a Fixed-Aperture Exhaust Nozzle Employing Fluidic Injection for Multiaxis Thrust Vector Control. AIAA 97-3149, July1997.
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