Application of Back-Step Coanda Flap for the Supersonic Co-flowing Fluidic Thrust Vector Control

Author:

Lee Yeol1,Song MyungJun1,Chang HongBeen1,Cho Yongho2

Affiliation:

1. Korea Aerospace University

2. Microfriend

Publisher

American Institute of Aeronautics and Astronautics

Reference19 articles.

1. 1Deere,K. A."SummaryofFluidicThrustVectoringResearchConductedatNASALangleyResearch Center,"AIAAPaper 2003-3800,2003.

2. 2Chiarelli, C., Johnsen, R. K., Shieh, C. F., Wing, D. J. "Fluidic Scale Model Multi-plane Thrust Vector Control Test Results,"AIAA Paper1993-2433,1993.

3. 3Diaz-Guardamino,I.E."CombiningSuctionControlandTransverseJets forFluidicThrustVectorControl,"ProQuest,MS Thesis,TheStateUniversityofNewYork, 2008.

4. 4Wing, D. J. "Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two-Dimensional Convergent Divergent Nozzle,"NASA Technical Memorandum4574,1994.

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