Journal of the Korean Society of Propulsion Engineers (한국추진공학회지)

The Korean Society of Propulsion Engineers (한국추진공학회)
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Research Activities on PGC Propulsion Based on RDE, Part II: Application Studies

RDE 기반 PGC 추진기관 연구 동향, Part II: 응용연구

  • Kim, Jung-Min (Department of Aerospace Engineering, Pusan National University) ;
  • Niyasdeen, Mohammed (Department of Aerospace Engineering, Pusan National University) ;
  • Han, Hyung-Seok (Department of Aerospace Engineering, Pusan National University) ;
  • Oh, Sejong (Department of Aerospace Engineering, Pusan National University) ;
  • Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University)
  • Received : 2016.12.29
  • Accepted : 2017.05.10
  • Published : 2017.12.01
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Abstract

The early basic studies on RDE has been surveyed in the previous paper. Recently active researches are carrying on for the application to the power plant and aerospace propulsion systems. Collaboration researches are going on for the application of RDE for the gas turbine, liquid rocket and combined cycle engines in many countries. Following the previous Part 1 paper, present paper is intended to provide the comprehensive survey of recent worldwide efforts on the realistic application of RDE.

앞서의 논문을 통하여 RDE와 관련된 초기의 기초 연구를 살펴보았다. 최근에는 이를 바탕으로 동력장치 및 항공우주 추진기관에 적용하기 위한 연구가 활발히 진행되고 있다. 각국에서는 대학과 기업 그리고 연구소의 공동 연구를 통하여 가스터빈 및 액체 로켓 엔진이나 복합사이클 엔진으로의 응용연구가 활발히 진행되고 있어, 본 논문에서는 앞서의 Part I 논문에 이어 세계 곳곳에서 진행되고 있는 실질적인 RDE 응용연구에 대한 포괄적인 고찰을 수행하였다.

Keywords

References

  1. Kim, J.H., Kim, T.Y., Jin, W.S. and Choi, J.Y., "Research Activities on PGC Propulsion Systems Based on PDE," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 10, pp. 858-869, 2014. https://doi.org/10.5139/JKSAS.2014.42.10.858
  2. Yi, T.H., Lou, J., Turangan, C., Choi, J.Y. and Wolanski, P., "Propulsive Performance of a Continuously Rotating Detonation Engine," Journal of Propulsion and Power, Vol. 27, No. 1, pp. 171-181, 2011. https://doi.org/10.2514/1.46686
  3. Braun, E.M., Lu, F.K., Wilson, D.R. and Camberos, J.A., "Airbreathing rotating detonation wave engine cycle analysis," Aerospace Science and Technology, Vol. 27, No. 1, pp. 201-208, 2013. https://doi.org/10.1016/j.ast.2012.08.010
  4. Braun, E.M., Lu, F.K. and Wilson, D.R., "Detonation Engine Performance Comparison Using First and Second Law Analysis," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, T.N., U.S.A., AIAA 2010-7040, Jul. 2010.
  5. Lu, F.K. and Braun, E.M., "Rotating detonation wave propulsion: experimental challenges, modeling, and engine concepts," Journal of Propulsion and Power, Vol 30, No. 5, pp. 1125-1142, 2014. https://doi.org/10.2514/1.B34802
  6. Schwer, D. and Kailasanath, K., "Numerical Investigation of Rotating Detonation Engines," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, T.N., U.S.A., AIAA 2010-6880, Jul. 2010.
  7. Schwer, D. and Kailasanath, K., "Numerical investigation of the physics of rotating-detonation-engines," Proceedings of the Combustion Institute, Vol. 33, No. 2, pp. 2195-2202, 2011. https://doi.org/10.1016/j.proci.2010.07.050
  8. Kailasanath, K., "The Rotating-Detonation-Wave Engine Concept: A Brief Status report," 49th AIAA Aerospace Sci. Meeting, Orlando, F.L., U.S.A., AIAA 2011-580, Jan. 2011.
  9. Nordeen, C.A., "Thermodynamics of a rotating detonation engine," Ph. D. Dissertation, Graduate School, University of Connecticut, Storrs, Mansfield, C.T., U.S.A., 2013.
  10. Schwer, D.A. and Kailasanath, K., "Numerical study of the effects of engine size on rotating detonation engines," 49th AIAA Aerospace Sciences Meeting, Orlando, F.L., U.S.A., AIAA 2011-581, Jan. 2011.
  11. Schwer, D.A. and Kailasanath, K., "Effect of inlet on fill region and performance of rotating detonation engines," 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conference, San Diego, C.A., U.S.A., AIAA 2011-6044, Jul. 2011.
  12. Stoddard, W. and Gutmark., E., "Comparative numerical study of RDE injection designs," 52nd AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, National Harbor, M.D., U.S.A., AIAA 2014-0285, Jan. 2014.
  13. Schwer, D.A. and Kailasanath., K, "Effect of Low Pressure Ratio on Exhaust Plumes of Rotating Detonation Engines," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, O.H., U.S.A., AIAA 2014-3901, Jul. 2014.
  14. Nordeen, C.A., Schwer, D. and Corrigan, A., "Area Effects on Rotating Detonation Engine Performance," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, Cleveland, O.H., U.S.A., AIAA 2014-3900, Jul. 2014.
  15. Paxson, D.E., "Numerical Analysis of a Rotating Detonation Engine in the Relative Reference Frame," 52nd AIAA Aerospace Sciences Meeting, National Harbor, M.D., U.S.A., AIAA 2014-0284, Mar. 2014.
  16. Fievisohn, R. and Yu, K., "Steady-State Analysis of Rotating Detonation Engine Flowfields with the Method of Characteristics," Journal of Propulsion And Power, Vol. 33, No. 1, pp. 89-99, 2017. https://doi.org/10.2514/1.B36103
  17. Sousa, J., Paniagua, G. and Morata, E.C., "Thermodynamic analysis of a gas turbine engine with a rotating detonation combustor," Applied Energy, Vol. 195, No.1 pp. 247-256, 2017. https://doi.org/10.1016/j.apenergy.2017.03.045
  18. Fujiwara, T., Hishida, M., Kindracki, J. and Wolanski, P., "Stabilization of detonation for any incoming Mach numbers," Combustion, Explosion, and Shock Waves, Vol. 45, No. 5, pp. 603-605, 2009. https://doi.org/10.1007/s10573-009-0072-y
  19. Wolanski, P., "Rotating detonation wave stability," 23rd ICDERS, Irvine, C.A., U.S.A., pp. 24-29, Jul. 2011.
  20. Hayashi, A.K., Kimura, Y., Yamada, T., Yamada, E., Kindracki, J., Dzieminska, E., Wolanski, P., Tsuboi, N., Tangirala, V. and Fujiwara, T., "Sensitivity analysis of Rotating detonation engine with a detailed reaction model," 47th AIAA Aerospace Sciences Meeting, Orlando, F.L., U.S.A., AIAA 2009-633, Jan. 2009.
  21. Yamada, T., Hayashi, K., Tsuboi, N., Yamada, E., Tangirala, V. and Fujiwara, T., "Numerical analysis of threshold of limit detonation in rotating detonation engine," 48th AIAA Aerospace Sciences Metting, Orlando, F.L., U.S.A., AIAA 2010-153, Jan. 2010.
  22. Uemura, Y., Hayashi, A.K., Asahara, M., Tsuboi, N. and Yamada, E., "Transverse Wave Generation Mechanism in Rotating Detonation," Proceedings of the Combustion Institute, Vol. 34, Issue 2, pp. 1981-1989, 2013. https://doi.org/10.1016/j.proci.2012.06.184
  23. Sichel, M. and Foster, J.C., "The ground impulse generated by a plane fuel-air explosion with side relief," Acta Astronautica, Vol. 6, Issues 3-4, pp. 243-256, 1979. https://doi.org/10.1016/0094-5765(79)90096-1
  24. Vasil'ev, A.A. and Zak, D.V., "Detonation of gas jets," Combustion, Explosion and Shock Waves, Vol. 22, No. 4, pp. 463-468, 1986. https://doi.org/10.1007/BF00862893
  25. Cho, K.Y., Codoni, J.R., Rankin, B.A., Hoke, J. and Schauer, F., "Effects of Lateral Relief of Detonation in a Thin Channel," 55th AIAA Aerospace Sciences Meeting, Grapevine, T.X., U.S.A., AIAA 2017-0373, Jan. 2017.
  26. Burr, J.R. and Yu, K.H., "Detonation Reignition within a Rotating Detonation Engine," 54th AIAA Aerospace Sciences Meeting, San Diego, C.A., U.S.A., AIAA 2016-1202, Jan. 2016.
  27. Masselot, D., Fievet, R. and Raman, V., "Effect of Equivalence Ratio and Turbulence Fluctuations on the Propagation of Detonations," 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Grapevine, T.X., U.S.A., AIAA 2017-0374, Jan. 2017.
  28. Lee, D.S., Shin, E.J.R., Won, S.H. and Choi, J.Y., "Ionization Characteristics of Noble Gases behind a Strong Shock Waves," 46th AIAA Aerospace and Science Meeting and Exhibit, Reno, N.V, U.S.A., AIAA 2008-1116, Jan. 2008.
  29. Kim, T.Y. and Choi, J.Y., "Numerical Study of Detonation Wave Propagation in 2-D Channels of Arbitrary Radius of Curvature," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, O.H., U.S.A., AIAA 2014-3903, Jul. 2014.
  30. Nakayama, H., Kasahara, J., Matsuo, A. and Funaki, I., "Front shock behavior of stable curved detonation waves in rectangular-cross-section curved channels," Proceedings of the Combustion Institute, Vol. 34, No. 2, pp. 1939-1947, 2013. https://doi.org/10.1016/j.proci.2012.06.012
  31. Sugiyama, Y., Nakayama, Y., Matsuo, A., Nakayama, H. and Kasahara, J., "Numerical investigations on detonation propagation in a two-dimensional curved channel," Combustion Science and Technology, Vol. 186, No. 10-11, pp. 1662-1679, 2014. https://doi.org/10.1080/00102202.2014.935621
  32. Jian, L., Jian, G., N., Hui, Z., Li, H. and Cheng, W., "Numerical Investigation on the Propagation Mechanism of Steady Cellular Detonations in Curved Channels," Chinese Physics Letters, Vol. 32, No. 4, pp. 048202, 2015. https://doi.org/10.1088/0256-307X/32/4/048202
  33. Short, M., Quirk, J.J., Meyer, C.D. and Chiquete, C., "Steady detonation propagation in a circular arc: a Detonation Shock Dynamics model," Journal of Fluid Mechanics, Vol. 807, pp. 87-134, 2016. https://doi.org/10.1017/jfm.2016.597
  34. Eude, Y., Davidenko, D., Falempin, F. and Gokalp, I., "Use of the adaptive mesh refinement for 3D simulations of a CDWRE (continuous detonation wave rocket engine)," 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, C.A., U.S.A., AIAA 2011-2236, Apr. 2011.
  35. Jiang, X.H., Fan, B.C., Gui, M.Y. and Chen, Z.H., "Numerical Investigation on The Three-Dimensional Flow Patterns of the Continuous Rotation Detonation," 22nd ICDERS, Minsk, Belarus, Vol. 182, pp. 1586-1597, Jul. 2009.
  36. Pan, Z., Fan, B., Zhang, X., Gui, M. and Dong, G., "Wavelet Pattern and Self-Sustained Mechanism of Gaseous Detonation Rotating in a Coaxial Cylinder," Combustion and Flame, Vol. 158, Issue 11, pp. 2220-2228, 2011. https://doi.org/10.1016/j.combustflame.2011.03.016
  37. Tang, X.M., Wang, J.P. and Shao, Y.T., "Three-Dimensional Numerical Investigations of The Rotating Detonation Engine with a Hollow Combustor," Combustion and Flame, Vol. 162, Issue 4, pp. 997-1008, 2015. https://doi.org/10.1016/j.combustflame.2014.09.023
  38. Choi, J.Y., "Discussions on the Combustion Dynamics of RDE with Relevance to the Liquid Rocket Combustion Instability," The 45th KOSCO Symposium, Pohang, Korea, Nov. 2012.
  39. Choi, J.Y., "PGC Research Progress in PNU & Perspectives on PGC Propulsion," AIAA Science and Technology Forum and Exposition 2014, National Harbor, M.D., U.S.A., Jan. 2014.
  40. Nicholls, J.A., Wilkinson, H.R. and MORRISON, R. B., "Intermittent detonation as a thrust-producing mechanism," Journal of Jet Propulsion, Vol. 27, No. 5, pp. 534-541, 1957. https://doi.org/10.2514/8.12851
  41. Falempin, F., Daniau, E., Getin, N., Bykovskii, F., and Zhdan, S., "Toward a continuous detonation wave rocket engine demonstrator," 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia, AIAA 2006-7959, Nov. 2006.
  42. Kindracki, J., Kobiera, A., Wolanski, P., Gut, Z., Folusiak, M. and Swiderski, K., "Experimental And Numerical Study of The Rotating Detonation Engine in Hydrogen-Air Mixture," Progress in Propulsion Physics, Vol. 2, pp. 555-582, 2011.
  43. Kindracki, J., "Experimental Research on Rotating Detonation in Liquid Fuel-Gaseous Air Mixture," Aerospace Science and Technology, Vol. 43, pp. 445-453, 2015. https://doi.org/10.1016/j.ast.2015.04.006
  44. Okninski, A., Marciniak, B., Barthowiak, B., Kaniewski, D., Matyszewski, J., Kindracki, J. and Wolanski, P., "Development of The Polish Small Sounding Rocket Program," Acta Astronautica, Vol. 108, pp. 46-56, 2015. https://doi.org/10.1016/j.actaastro.2014.12.001
  45. Okninski, A., Kindracki, J. and Wolanski P., "Rocket Rotating Detoantion Engine Flight Demonstrator," Aircraft Engineering and Aerospace Technology, Vol. 88, Issue. 4, pp. 480-491, 2016. https://doi.org/10.1108/AEAT-07-2014-0106
  46. Nakagami, S., Matsuoka, K., Kasahara, J., Kumazawa, Y., Fujii, J., Matsuo, A. and Funaki, I., "Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor," Journal of Propulsion and Power, Vol. 33, No. 1, pp. 80-88, 2016.
  47. Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A. and Funaki, I., "Experimental study of the structure of forward-tilting rotating detonation waves and highly maintained combustion chamber pressure in a disk-shaped combustor," Proceedings of the Combustion Institute, Vol. 36, No. 2, pp. 2673-2680, 2017. https://doi.org/10.1016/j.proci.2016.07.097
  48. Kasahara, J., Kato, Y., Ishihara, K., Matsuoka, K., Matsuo, A., Funaki, I., Nakata, D., "Research and Development of Rotating Detonation Engine for Upper-Stage Kick Motor System," IWDP, Nanyang, Singapore, Jul. 2016.
  49. "Russia was the first to successfully test the detonation liquid rocket engine of a new generation on environmentally friendly fuel," 26 Aug. 2017, retrieved 15 Mar. 2017 from World Wide Web location http://fpi.gov.ru/press/news/20160826.
  50. Wolanski, P., "Experimental and Numerical Research of Continuous Rotating Detonation in Poland," IWDP, Tsukuba, Japan, Sep. 2012.
  51. Wolanski, P., "Research on RDE in Poland," IWDP, Tainan, Taiwan, Jul. 2013.
  52. Wolanski, P., Kindracki, J., Fujiwara, T., Oka, Y. and Shima-uchi, K., "An Experimental Study of Rotating Detonation Engine," Proc. 20th ICDERS, Montreal, Canada, ICDERS 2005-107, Jul. 2005.
  53. Heister, S. and Slabaugh, C., "Advancing Pressure Gain Combustion in Terrestrial Turbine Systems," University Turbine Systems Workshop, Atlanta, G.A., U.S.A., Nov. 2015.
  54. Claflin, S., "New and Existing Systems Show Progress," Aerospace America, AIAA, Vol. 11, 2016.
  55. Ferguson, d., Sidwell, T., Roy, A., Strakey, P., Bedick, C., O'Meara, B. and Billups, D., "Overview of Pressure Gain Combustion Studies at NETL," University Turbine System Research Project Review Meeting, Blacksburg, V.A., U.S.A., Nov. 2016.
  56. "Pressure Gain Combustion," retrieved 3 Apr. 2017 from World Wide Web location https://www.netl.doe.gov/research/coal/energy-systems/turbines/pressure-gaincombustion.