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http://dx.doi.org/10.6108/KSPE.2013.17.2.084

Experimental Study of the Thrust Vectoring Characteristics in a Two-Dimensional Convergent-Divergent Nozzle  

Yu, Du Whan (전북대학교 항공우주공학과)
Choi, Seong Man (전북대학교 항공우주공학과)
Oh, Seong Hwan (국방과학연구소 7기술연구본부 2부)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.17, no.2, 2013 , pp. 84-93 More about this Journal
Abstract
Stealthy, high maneuverability and super cruise abilities are required for the next generation fighter and unmanned aircraft. Thrust vector control technique currently come into use to meet these requirements. In this experimental study, axial and pitch thrust were measured and Schlieren visualization were carried out using the scaled two dimensional thrust vector nozzles under various pitch deflection angle, pitch flap length and height. From the study, we could get the supersonic flow characteristics and draw an optimum geometric configuration of the two dimensional thrust vector nozzle.
Keywords
2-D C-D Nozzle; Thrust Vector; Pitch Deflection;
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1 Stevens, H. L., Thayer, E. B., and Fullerton, J. F., "Development of the Multi- Function 2-D/C-D Nozzle," AIAA/SAE/ASME 17th Joint Propulsion Conference, AIAA-81-1491, 1981, pp.1-11
2 김윤희, 최성만, 장현수, "2D 추력편향 노즐 성능 및 유동 해석," 한국추진공학회 제33회 추계학술대회논문집, 2009, pp.483-486
3 이종성, Vicent Lijo, 김희동, "과팽창 노즐에 서 발생하는 충격파-경계층 간섭의 천이에 관한 수치 해석적 연구," 대한기계학회 유체 공학부문 춘계학술대회 논문집, 2010, pp.157-162
4 Taylor, J. G., "A Static Investigation of a Simultaneous Pitch and Yaw Thrust Vectoring 2-D C-D Nozzle," AIAA/ ASME/SAE/ASEE 24th Joint Propulsion Conference, 1988, pp.1-12
5 Yagle, P. J., Miller, D. N., Ginn K. B., and Hamstra, J. W., "Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles," Journal of Engineering for Gas Turbines and Power, Vol. 123, No. 3, 2001, pp.502-507   DOI   ScienceOn
6 Porzio, A. J. and Franke, M. E., "Experimental Study of a Confined Jet Thrust Vector Control Nozzle," Journal of Propulsion and Power, Vol. 5, No. 5, 1989, pp.596-601   DOI   ScienceOn
7 Deere, K. A., "Summary of Fluidic Thrust Vectoring Research Conducted at NASA LANGLEY Research Center," The 21st AIAA Applied Aerodynamics Conference, AIAA-2003-3800, 2003, pp.1-18
8 Brenner, M. J., "Aeroservoelastic Modeling and Validation of a Thrust -Vectoring F/A-18 Aircraft," NASA Technical Paper 3647, 1996
9 신춘식, 김희동, "이중목 노즐을 이용한 추력 벡터 제어에 관한 기초적 연구," 한국 추진 공학회지, 제14권, 제6호, 2010, pp.25-30
10 전동현, 이열, 허준영, 성홍계, 전동연, "Coanda 효과를 이용한 추력편향 제어에 관한 실험적 연구," 한국항공우주학회 2008년도 추계학술발표회 논문집, 2008, pp.82-85
11 Carson, G. T. Jr. and Capone, F. J., "Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-Vectoring Capability," NASA Technical Memorandum 4237, 1991
12 Herbst, W. B., "Future Fighter Technologies," Journal of Aircraft, Vol. 17, No. 8, 1980, pp.561-566   DOI   ScienceOn