597
Views
83
CrossRef citations to date
0
Altmetric
Original Articles

Experimental Realization of H2/Air Continuous Rotating Detonation in a Cylindrical Combustor

, , , &
Pages 1302-1317 | Received 22 Jun 2011, Accepted 02 Apr 2012, Published online: 23 Aug 2012

REFERENCES

  • Bykovskii , F.A. , Klopotov , I.D. , and Mitrofanov , V.V. 1975 . Spin detonation of gases in a cylindrical combustor . Dokl. Akad. Nauk , 224 , 1038 – 1041 .
  • Bykovskii , F.A. , and Mitrofanov , V.V. 1980. Detonation combustion of a gas mixture in a cylindrical chamber. Combustion, Explosion, and Shock Waves , 16, 570–578.
  • Bykovskii , F.A. , and Vedernikov , E.F. 2003 . Continuous detonation of a subsonic flow of a propellant . Combustion, Explosion, and Shock Waves , 39 , 323 – 334 .
  • Bykovskii , F.A. , Zhdan , S.A. , and Vedernikov , E.F. 2006a . Continuous spin detonations . J. Propul. Power , 22 , 1204 – 1216 .
  • Bykovskii , F.A. , Zhdan , S.A. , and Vedernikov , E.F. 2006b . Continuous spin detonation of fuel-air mixtures . Combustion, Explosion, and Shock Waves , 42 , 463 – 471 .
  • Bykovskii , F.A. , Zhdan , S.A. , and Vedernikov , E.F. 2008 . Continuous spin detonation of Hydrogen-oxygen mixtures, 1: Annular cylindrical combustors . Combustion, Explosion, and Shock Waves , 44 , 150 – 162 .
  • Dabora , E.K. , Nicholls , J.A. , and Morrison , R.B. 1965 . The influence of a compressible boundary on the propagation of gaseous detonations . Symp. (Int.) Combust. , 817 – 830 .
  • Hishida , M. , Fujiwara , T. , and Wolanski , P. 2009 . Fundamentals of rotating detonations . Shock Waves , 19 , 1 – 10 .
  • Kindracki , J. , Wolanski , P. , and Gut , Z. 2011 . Experimental research on the rotating detonation in gaseous fuels-oxygen mixtures . Shock Waves , 21 , 75 – 84 .
  • Liu , S.-j. , Lin , Z.-y. , Sun , M.-B. , and Liu , W.-D. 2011 . Thrust vectoring of a continuous rotating detonation engine by changing the local injection pressure . Chin. Phys. Lett. , 28 , 094704 .
  • Lu , F.K. , Braun , E.M. , Massa , L. , and Wilson , D.R. 2011 . Rotating detonation wave propulsion: Experimental challenges, modeling, and engine concepts (Invited) . AIAA paper no. 2011–6043.
  • Naour , B.L. , Falempin , F. , and Miquel , F. 2011 . Recent experimental results obtained on continuous detonation wave engine . AIAA paper no. 2011–2235.
  • Nicholls , J.A. , Cullen , R.E. , and Ragland , K.W. 1966 . Feasibility studies of a rotating detonation wave rocket motor . Journal of Spacecraft and Rockets , 3 , 893 – 898 .
  • Russo , R.M. , King , P.I. , Schauer , F.R. , and Thomas , L.M. 2011 . Characterization of pressure rise across a continuous detonation engine . AIAA paper no. 2011–6046.
  • Schwer , D. , and Kailasanath , K. 2011 . Numerical investigation of the physics of rotating-detonation-engines . Proc. Combust. Inst. , 33 , 2195 – 2202 .
  • Shao , Y.T. , Liu , M. , and Wang , J.P. 2010 . Numerical investigation of rotating detonation engine propulsive performance . Combust. Sci. Technol. , 182 , 1586 – 1597 .
  • Voitsekhovskii , B.V. 1959 . Maintained detonations . Dokl. Akad. Nauk , 129 , 1254 – 1256 .
  • Voitsekhovskii , B.V. 1960 . Spinning maintained detonations . Prikl. Mekh. Tekh. Fiz. , 157 – 164 .
  • Yamada , T. , Hayashi , A.K. , Yamada , E. , Tsuboi , N. , Tangirala , V.E. , and Fujiwara , T. 2010 . Detonation limit thresholds in H2/O2 rotating detonation engine . Combust. Sci. Technol. , 182 , 1901 – 1914 .

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.