Performance Analyses of Fluidic Thrust Vector Control System Using Dual Throat Nozzle
Author:
Affiliation:
1. Okayama University of Science, Okayama 700-0005, Japan
2. Chuo Engineering, Co., Ltd., Tokyo 102-0083, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059696
Reference18 articles.
1. DeereK. A.BerrierB. L.FlammJ. D.JohnsonS. K. “A Computational Study of a New Dual Throat Fluidic Thrust Vectoring Nozzle Concept,” AIAA Paper 2005-3502, July 2005. 10.2514/6.2005-3502
2. FlammJ. D.DeereK. A.BerrierB. L.JohnsonS. K.MasonM. L. “Experimental Study of a Dual-Throat Fluidic Thrust-Vectoring Nozzle Concept,” AIAA Paper 2005-3503, July 2005. 10.2514/6.2005-3503
3. Design Enhancements of the Two-Dimensional, Dual Throat Fluidic Thrust Vectoring Nozzle Concept
4. FlammJ. D.DeereK. A.MasonM. L.BerrierB. L.JohnsonS. K. “Experimental Study of an Axisymmetric Dual Throat Fluidic Thrust Vectoring Nozzle for Supersonic Aircraft Application,” AIAA Paper 2007-5084, July 2007. 10.2514/6.2007-5084
5. BellandiE. G.SlippeyA. J. “Preliminary Analysis and Design Enhancements of a Dual-Throat FTV Nozzle Concept,” AIAA Paper 2009-3900, June 2009. 10.2514/6.2009-3900
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