Application of Backstep Coanda Flap for Supersonic Coflowing Fluidic Thrust-Vector Control
Author:
Affiliation:
1. Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang-si 412-791, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052971
Reference18 articles.
1. DeereK. A. “Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center,” AIAA Paper 2003-3800, June 2003.
2. WingD. J. “Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two-Dimensional Convergent Divergent Nozzle,” NASA TM-4574, 1994.
3. Counterflow thrust vectoring of supersonic jets
4. Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet
5. Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles
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