Acknowledgement
이 논문은 국방과학연구소가 지원하는 저피탐무인항공기 추진계통 IR 감소 기술 연구로 수행되었습니다.
References
- L. Bougas., M. Hornung, "Propulsion system intergration and thrust vectoring aspect for scaled jet UAVs, CEAS Aeronaut. Journal, Vol. 4 pp. 327-343, 2013. https://doi.org/10.1007/s13272-013-0076-x
- W.M. Presz. G. Reynolds. D.C. McCormick, "Thrust augment using mixer-ejectordiffuser systems," AIAA, 40th AIAA Sciences Meeting & Exhibit, Reno, NV, pp. 94-0020, January 2002.
- Brian J. Tester and Michael J. Fisher, "A contribution to the understanding and prediction of jet noise generation in forced mixer," 12th AIAA/CEAS Aeroacoustics Conference, Cambridge Massachusetts, pp. 2006-2542, May 2006.
- Pelt HV, Neely A, Young J., "A system study on fluidic thrust vectoring," 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conferences, Glasgow, Scotland, AIAA paper 2015-3565, July 06-09, 2015.
- Cen Z., Smith T., Stewart P., Steart J, "Intergrated flight/thrust vectroing control for jet-powerd unmanned aerial vehicles with ACHEON propulsion," Journal of Aerospace Engineering, Vol. 229, No. 5, pp. 1057-75, 2015.
- B.L. Berrier., M.L. Mason, "Static performance of an axisymmetric nozzle with post-exit vanes for multi axis thrust vectoring, in: NASA TP-2800, 1988.
- D.J Wing., C.T.L., Mills., M.L. Mason, "Static investigation of a multi axis thrust vectoring nozzle with variable internal contouring ability," NASA TP-3628, 1997.
- K.A.Deere., B.L. Berrier., J.D. Flamm., S.K. Johnson, "Computational study of fluidic thrust vectoring using separation control in a nozzle," The 21st AIAA Applied Aerodynamics Conference, pp. 3803, 2003.
- Farzad Forghany, Mohammad Taeibe Rahni and Abdollah Asdollahi Ghohieh, "Numerical investigation of freestream flow effects on thrust vector control performance," Ain Shams Engineering Journal, Vol. 9, pp. 3293-3303, 2018. https://doi.org/10.1016/j.asej.2017.12.004
- T.Chandra Sekar., A.Kushari., B.Mody., B.Uthup, "Fluidic thrust vectoring using transverse jet injection in a convergin nozzle with Aft-deck," Experimental Thermal and Fluid Science, Vol. 86, pp. 189-203, 2017. https://doi.org/10.1016/j.expthermflusci.2017.04.017
- P.Behrouzi and J.J. McGuirk., "Underexpanded jet development from a rectangular nozzle with Aft-deck," AIAA Journal, Vol. 53, No. 5, pp. 1287-1298, 2015. https://doi.org/10.2514/1.J053376
- Miau. J.J., Leu, T.S., Chou, J.H., and Lin, S. A., "Flow Distortion a Circular-to-Rectangular Transition Duct," AIAA Journal, Vol. 28, No. 8, 1990, pp. 1447-1456. https://doi.org/10.2514/3.25237
- Hyun-Jin Lee, Ji-Hyun Lee, Rho-Shin Myong, Sun-Mi Kim, Sung-Man Choi, Won-Cheol Kim., "Computational and Experimental Investigation of Thermal Flow Field of Micro Turbojet Engine with Various Nozzle Configurations," The Korean Society for Aeronautical & Space Sciences, Vol. 46, No. 2, 2018, pp. 150-158. https://doi.org/10.5139/JKSAS.2018.46.2.150
- Hyun-Jin Lee, Ji-Hyun Lee, Rho-Shin Myong, Sun-Mi Kim, Sung-Man Choi, Won-Cheol Kim, "Computational and Experimental Investigation of Thermal Flow Field of Micro Turbojet Engine with Various Nozzle Configurations," The Korean Society for Aeronautical & Space Sciences, Vol. 46, No. 2, 2018, pp. 150-158. https://doi.org/10.5139/JKSAS.2018.46.2.150
- Meng Sing Liou, "A sequel to AUSM, Part II: AUSM+-up for all speeds," Journal of Computational Physics, Vol. 129, Issue. 2, pp 364-382, 1996. https://doi.org/10.1006/jcph.1996.0256
- Sun, X.-L., Wang, Z.-X., Zhou, L., Shi, J.-W., and Liu, Z.-W., "Influences of Design Parameters on a Double Serpentine Convergent Nozzle," Journal of Engineering for Gas Turbines and Power, Vol. 138, No. 7, pp. 072301-072316, 2016. https://doi.org/10.1115/1.4032338
- C.-M. HO, E, Gutmark, "Vortex induction and mass entrainment in a small aspect ratio elliptic jet," J. Fluid Mech. 1987.