368
Views
28
CrossRef citations to date
0
Altmetric
Articles

Ethylene Continuous Rotating Detonation in optically accessible racetrack-like combustor

, &
Pages 676-695 | Received 01 Nov 2017, Accepted 05 Jul 2018, Published online: 19 Jul 2018

References

  • Beeson, H.D., Clenagan, M., Bishop, C.V., Benz, F.J., Pitz, W.J., Westbrook, C.K., and Lee, J.H.S. 1991. Detonability of hydrocabon fuels in air. Astronaut. Aeronaut., 133:19.
  • Bykovskii, F.A., Zhdan, S.A., and Vedernikov, E.F. 2006. Continuous spin detonations. J. Propul.Power, 22, 1204–1216.
  • Cho, K.Y., Codoni, J.R., Rankin, B.A., Hoke, J.L., and Schauer, F.R. (2016). High-repetition-rate chemiluminescence imaging of a rotating detonation engine, AIAA 2016-1648. 54th AIAA, California, January 4-8.
  • Dyer, R., Naples, A., Kaemming, T., Hoke, J., and Schauer, F. (2012). Parametric testing of a unique rotating detonation engine design, AIAA 2012-0121. 50th AIAA. Nashville, Tennessee, January 9-12.
  • Frolov, S.M., Aksenov, V.S., Dubrovskii, A.V., Ivanov, V.S., and Shamshin, I.O. 2015a. Energy Efficiencyof a continuous-detonation combustion chamber. Combustion, Explosion, and Shock Waves, 51(2), 232–245.
  • Frolov, S.M., Aksenov, V.S., Ivanov, V.S., and Shamshin, I.O. 2015b. Large-scale hydrogeneair continuous detonation combustor. Int. J. Hydrogen Energy, 40, 1616–1623.
  • Ishihara, K., Kato, Y., Ken, M., Kasahara, J., Matsuo, A., and Funaki, I. (2015). Performance evaluation of a rotating detonation engine with conical-shape tail, AIAA 2015-0630. 53rd AIAA. Kissimmee, Florida, January 5-9.
  • Kato, Y., Ishihara, K., Gawahara, K., Matsuoka, K., Kasahara, J., and Matsuo, A. (2014). Thrust measurement of rotating detonation engine by sled test, AIAA 2014-4034. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, July 28-30.
  • Kindracki, J., Wola´Nski, P., and Gut, Z. 2011. Experimental research on the rotating detonation in gaseous fuels–oxygen mixtures. Shock Waves, 21, 75–84.
  • Kindracki, J. 2015. Experimental research on rotating detonation in liquid fuel–gaseous air mixtures. Aerospace Science and Technology, 43, 445–453.
  • Le Naour, B., Falenmpin, F., and Miquel, F. (2011). Recent experimental results obtained on continuous detonation wave engine, AIAA 2011-2235. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California, April 11-14.
  • Liu, S.J., Lin, Z.Y., Liu, W.D., Lin, W., and Sun, M.B. 2012. Experimental and three-dimensional numerical investigations on H2/air continuous rotating detonation wave. Proc. Inst. Mech. Eng., 227(2), 326–341.
  • Liu, S.J., Liu, W.D., Lin, Z.Y., and Lin, W. 2015. Experimental research on the propagation characteristics of continuous rotating detonation wave nearthe operating boundary. Combust. Sci. Technol., 187(11), 1790–1804.
  • Rankin Brent, A., Fugger Christopher, A., Richardson Daniel, R., Cho Kevin, Y., Hoke John, L., Caswell Andrew, W., Gord James, R., and Schauer Frederick, R. (2016). Evaluation of mixing processes in a non-premixed rotating detonation engine using acetone PLIF imaging, AIAA 2016-1198. 54th AIAA, San Diego, California, January 4-8.
  • Rankin Brent, A., Richardson Daniel, R., Caswell Andrew, W., Naples Andrew, G., Hoke John, L., and Schauer Frederick, R. 2017. Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine. Combust. Flame, 176, 12–22.
  • Schwer Douglas, A., and Kailas, K. (2012). Feedback into mixture plenums in rotating detonation engines, AIAA 2012-0617. 50th AIAA. Nashville, Tennessee, January 9-12.
  • Soma, N., Ken, M., Jiro, K., Akiko, M., and Funaki, I. 2017. Experimental study of the structure of forward-tilting rotating detonation waves and highly maintained combustion chamber pressure in a disk-shaped combustor. Proc. Combust. Inst., 36, 2673–2680.
  • St. George, A., Driscoll, R., Anand, V., Munday, D., and Gutmark Ephraim, J. (2015). Fuel blending as a means to achieve initiation in a rotating detonation engine, AIAA 2015-0633. 53rd AIAA, Kissimmee, Florida, January 5-9.
  • Thomas Levi, M., Schauer Frederick, R., Hoke John, L., and Andrew, N. (2011). Buildup and operation of a rotating detonation engine, AIAA 2011-602. 49th AIAA, Orlando, Florida, January 4-7.
  • Voitsekhovskii, B.V. 1960. Stationary spin detonation. Soviet J. Appl. Mechanics Tech. Phys., 3, 157–164.
  • Wang, C., Liu, W.D., Liu, S.J., Jiang, L.X., and Lin, Z.Y. 2015a. Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen. Int. J. Hydrogen Energy, 40, 9530–9538.
  • Wang, C., Liu, W.D., Liu, S.J., Jiang, L.X., and Lin, Z.Y. 2015b. Experimental investigation on detonation combustion patterns of hydrogen/vitiated air within annular combustor. Exp. Thermal Fluid Sci., 66, 269–278.
  • Wilhite, J., Driscoll, R., St George, A., Anand, V., and Gutmark, E.J. (2016). Investigation of a rotating detonation engine using ethylene-air mixtures, AIAA 2016-1650. 54th AIAA, California, January 4-8.
  • Yi, T.-H., Lou, J., Turangan, C., Choi, J.-Y., and Wolanski, P. 2011. Propulsive performance of a continuously rotating detonation engine. J. Propul.Power, 27, 171–181.
  • Zhang, H.L., Liu, W.D., and Liu, S.J. 2016. Effects of inner cylinder length on H2/air rotating detonation. Int. J. Hydrogen Energy, 40, 13281–13293.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.