DOI QR코드

DOI QR Code

Research Activities on PGC Propulsion based on RDE, Part I: Basic Studies

RDE 기반 PGC 추진기관 연구 동향, Part I: 기초연구

  • 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 : 2017.10.01

Abstract

Fluid dynamic constant volume combustion technology detonation has been paid attention as a "game-changing" technology to overcome the efficiency and performance limitation of the present constant pressure combustion systems. For the past several years, a number of experimental and CFD-based theoretical studies have been conducted for the basic operation tests of RDE's. Present paper include a comprehensive survey on the research activities on RDE and its core technologies comprehensively to provide a direction for the future RDE researches, yet unfamiliar domestically.

데토네이션을 이용한 유체역학적 정적연소 기술은 현재의 정압연소 시스템의 효율 및 성능 한계를 극복할 수 있는 획기적 미래 추진 기술로 주목받고 있다. 지난 수년간 RDE의 기초적인 작동 실험과 CFD를 이용한 이론 분석 등 수많은 연구가 진행되었다. 본 논문에서는 아직 부족한 국내 RDE 연구에 참고가 되고자하는 목적으로 근래의 세계 각지에서 수행되고 있는 RDE 연구의 동향 및 핵심 기술에 대한 포괄적 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. First Holzwarth Experiment Gas Turbine, 1908, Deutsches Museum, 31 Jan. 2017 from http://www.deutsches-museum.de/en/collections/machines/power-engines/gas-turbines/holzwarth-gas-turbine-1908/.
  3. Gunston, B., "Napier Nomad: An engine of outstanding efficiency," Flight, Apr. 1954, pp. 543-551, Retrieved 18 Dec. 2009.
  4. Paxson, D., "Pressure-Gain Combustion for the Gas Turbine," University Turbine Systems Research Workshop, Pennsylvania State University, P.A., U.S.A., 2010.
  5. Kindracki, J., Kobiera, A. and Wolanski, P., "Experimental and numerical research on rotating detonation in a small rocket engine model," Silniki Spalinowe, Vol. 48, pp. 392-400, 2009.
  6. Kindracki, J., Institute of Heat Engineering, WUT, project no. UMO-2012/05/D/ST8/02308, granted by National Science Centre, Poland.
  7. Soloukhin, R.I., "Detonation Waves in Gases," Soviet Physics Uspekhi, Vol. 6, No. 4, pp. 523-539 1964. https://doi.org/10.1070/PU1964v006n04ABEH003586
  8. Voitsekhovskii, B.V., Mitrofanov, V.V. and Topchiyan, M.E., "Fizika Goreniya i Vzryva," Siberian Branch of the Russian Academy of Sciences, Vol. 5, No.3, pp. 385-395, 1969.
  9. Voitsekhovskii, B.V., Mitrofanov, V.V. and Topchiyan., M. E., "Structure of the detonation front in gases (survey)," Combustion, Explosion, and Shock Waves, Vol. 5, No. 3, pp. 267-273, 1969. https://doi.org/10.1007/BF00748606
  10. Bykovskii, F.A. and Mitrofanov, V.V., "Detonation combustion of a gas mixture in a cylindrical chamber," Combustion, Explosion, and Shock Waves, Vol. 16, No. 5, pp. 570-578, 1980. https://doi.org/10.1007/BF00794937
  11. Bykovskii, F.A., Vasil'ev, A.A., Vedernikov, E.F. and Mitrofanov, V.V., "Explosive combustion of a gas mixture in radial annular chambers," Combustion, Explosion and Shock Waves, Vol. 30, No. 4, pp. 510-516, 1994. https://doi.org/10.1007/BF00790158
  12. Bykovskii, F.A., Mitrofanov, V.V. and Vedernikov, E.F., "Continuous detonation combustion of fuel-air mixtures," Combustion, Explosion and Shock Waves, Vol. 33, No. 3, pp. 344-353, 1997. https://doi.org/10.1007/BF02671875
  13. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, E.F., "Continuous spin detonation in ducted annular combustors," Application of Detonation to Propulsion, pp. 174-179, 2004.
  14. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, E.F., "Spin detonation of fuel-air mixtures in a cylindrical combustor," Doklady Physics, Vol. 50, No. 1, pp. 56-58, 2005. https://doi.org/10.1134/1.1862376
  15. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, E.F., "Continuous spin detonation in annular combustors," Combustion, Explosion and Shock Waves, Vol. 41, No. 4, pp. 449-459, 2005. https://doi.org/10.1007/s10573-005-0055-6
  16. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, E.F., "Continuous spin detonations," Journal of Propulsion and Power, Vol. 22, No. 6, pp. 1204-1216, 2006. https://doi.org/10.2514/1.17656
  17. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, E.F., "Continuous spin detonation of fuel-air mixtures," Combustion, Explosion and Shock Waves, Vol. 42, No. 4, pp. 463-471, 2006. https://doi.org/10.1007/s10573-006-0076-9
  18. Bykovskii, F.A., Zhdan, S.A. and Vedernikov., E.F., "Continuous spin detonation of hydrogen-oxygen mixtures. 1. Annular cylindrical combustors," Combustion, Explosion, and Shock Waves, Vol. 44, No. 2, pp. 150-162, 2008. https://doi.org/10.1007/s10573-008-0021-1
  19. Bykovskii, F.A., Zhdan, S.A. and Vedernikov, F.F., "Continuous spin and pulse detonation of hydrogen-air mixtures in supersonic flow generated by a detonation wave," 22nd ICDERS, Minsk, Belarus, ICDES 2009-0024, Jul. 2009.
  20. Bykovskii, F.A. and Zhdan, S.A., "Continuous Spin Detonation of a Hydrogen - Air Mixture in the Air Ejection Mode," Detonation Wave Propulsion Workshop 2011, Bourges, France, pp. 11-13, 2011.
  21. Zhdan, S.A., "Mathematical model of continuous detonation in an annular combustor with a supersonic flow velocity," Combustion, Explosion, and Shock Waves, Vol. 44, No. 6, pp. 690-697, 2008. https://doi.org/10.1007/s10573-008-0104-z
  22. Zhdan, S.A., Bykovskii, F.A. and Vedernikov, E.F., "Mathematical modeling of a rotating detonation wave in a hydrogen-oxygen mixture," Combustion, Explosion, and Shock Waves, Vol. 43, No. 4, pp. 449-459, 2007. https://doi.org/10.1007/s10573-007-0061-y
  23. Cullen, R.E., Nicholls, J.A. and Ragland., K. W, "Feasibility studies of a rotating detonation wave rocket motor," Journal of Spacecraft and Rockets, Vol. 3, No. 6, pp. 893-898, 1966. https://doi.org/10.2514/3.28557
  24. 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
  25. Adamson, T.C. and Olsson, G.R., "Performance analysis of a rotating detonation wave rocket engine," Astronautica Acta, Vol. 13, No. 4, pp. 405, 1967.
  26. Lentsch, A., Bec, R., Serre, L., Falempin, F., Daniau, E., Piton, D., Prigent, A., Canteins, G., Zitoun, R., Desbordes, D., Jouot, F. and Gokalp, I., "Overview of current French activities on PDRE and continuous detonation wave rocket engines," CIRA, International Space Planes and Hypersonics Systems and Technologies Conference, Capua, Italy, AIAA 2005-3232, 2005.
  27. 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, 2006.
  28. Canteins, G., "Etude de la detonation continue rotative-Application a la propulsion," Ph. D. Dissertation, Faculte des Sciences Fondamentales et Appliquees, University of Poitiers, Poitiers, France, 2006.
  29. Davidenko, D., Gokalp, I. and Kudryavtsev, A., "Numerical Simulation of H2/O2 Continuous Spin Detonation with a Detailed Chemical Mechanism," 21st ICDERS, Poitiers, France, Jul. 2007.
  30. 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.
  31. Wolanski, P., Kindracki, J. and Gut, Z., "Experimental Research on The Rotating Detonation in Gaseous Fuel-Oxygen Mixture," Shock Waves, Vol. 21, pp. 75-84, 2011. https://doi.org/10.1007/s00193-011-0298-y
  32. 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.
  33. 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
  34. Hishida, M., Fujiwara, T. and Wolanski, P., "Fundamentals of rotating detonation," Shock Waves, Vol. 19, pp. 1-10, 2009. https://doi.org/10.1007/s00193-008-0178-2
  35. Naples, A., "Recent Progress in Detonation," IWDP, 2011.
  36. Theuerkauf, S.W., "Heat Exchanger Design and Testing for a 6-inch Rotating Detonation Engine," MS Thesis, AFIT-ENY-13-M33, Air Force Institute of Technology, 2013.
  37. Roy, A., Bedick, C., Strakey, P., Sidwell, T., Ferguson, D., Sisler, A. and Nix, A., "Development of a Three-dimensional Transient Wall Heat Transfer Model of a Rotating Detonation Combustor," 54th AIAA Aerospace Sciences Meeting, San Diego, C.A., U.S.A., AIAA 2016-0902, Jan. 2016.
  38. Fievisohn, R., "Rotating Detonation Engine Research at AFRL," IWDP, 2012.
  39. Claflin, S., "Recent Progress in Continuous Detonation Engine Development at Pratt & Whitney Rocketdyne," IWDP, 2013.
  40. 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.
  41. Gawahara, K., Nakayama, H., Kasahara, J., Matsuoka, K., Tomioka, S., Hiraiwa, T., Matsuo, A. and Funaki, I., "Detonation engine development for reaction control systems of a spacecraft," 49th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference, San Jose, C.A., U.S.A., Jul. 2013.
  42. Kato, Y., Gawahara, K., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Higashino, K. and Tanatsugu, N., "Thrust measurement of rotating detonation engine by sled test," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, O.H., U.S.A., AIAA 2014-4034, Jul. 2014.
  43. Ashida, T. and Kasahara, J., "Study on Detonation Engine Momentum and Thrust loss Measurement by Ballistic Pendulum and Laser Displacement Method," 52nd Aerospace Sciences Meeting, AIAA SciTech Forum, Harbor, M.D., U.S.A., AIAA 2014-1016, Jan. 2014.
  44. Wei, L., Jin, Z., Shijie, L. and Zhiyong, L., "An Experimental Study on $CH_4/O_2$ Continuously Rotating Detonation Wave in a Hollow Combustion Chamber," Experimental Thermal and Fluid Science, Vol. 62, pp. 122-130, 2015. https://doi.org/10.1016/j.expthermflusci.2014.11.017

Cited by

  1. The Experimental Study about the Effect of Operating Conditions on Multi-tube Pulse Detonation Engine Performance vol.19, pp.1, 2018, https://doi.org/10.1007/s42405-018-0026-2