Browse > Article
http://dx.doi.org/10.6108/KSPE.2017.21.6.091

Research Activities on PGC Propulsion Based on RDE, Part II: Application Studies  

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)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.21, no.6, 2017 , pp. 91-102 More about this Journal
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.
Keywords
Rotating Detonation Engine(RDE); Constant Volume Combustion(CVC); Pressure Gain Combustion(PGC);
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 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.
2 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.
3 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.   DOI
4 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.   DOI
5 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.   DOI
6 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.   DOI
7 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.
8 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.
9 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.   DOI
10 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.   DOI
11 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.
12 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.
13 Kindracki, J., "Experimental Research on Rotating Detonation in Liquid Fuel-Gaseous Air Mixture," Aerospace Science and Technology, Vol. 43, pp. 445-453, 2015.   DOI
14 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.   DOI
15 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.
16 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.
17 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.   DOI
18 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.   DOI
19 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.   DOI
20 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.
21 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.   DOI
22 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.   DOI
23 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.
24 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.   DOI
25 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.
26 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.   DOI
27 Wolanski, P., "Experimental and Numerical Research of Continuous Rotating Detonation in Poland," IWDP, Tsukuba, Japan, Sep. 2012.
28 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.   DOI
29 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.
30 "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.
31 Wolanski, P., "Research on RDE in Poland," IWDP, Tainan, Taiwan, Jul. 2013.
32 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.
33 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.
34 Claflin, S., "New and Existing Systems Show Progress," Aerospace America, AIAA, Vol. 11, 2016.
35 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.
36 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.
37 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.
38 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.
39 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.
40 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.
41 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.
42 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.
43 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.   DOI
44 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.
45 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.   DOI
46 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.   DOI
47 Wolanski, P., "Rotating detonation wave stability," 23rd ICDERS, Irvine, C.A., U.S.A., pp. 24-29, Jul. 2011.
48 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.
49 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.   DOI
50 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.   DOI
51 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.   DOI
52 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.
53 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.
54 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.
55 "Pressure Gain Combustion," retrieved 3 Apr. 2017 from World Wide Web location https://www.netl.doe.gov/research/coal/energy-systems/turbines/pressure-gaincombustion.
56 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.