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Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5

  • Published:2022-07 Issue: Volume:126 Page:107602
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Ivanov V.S.,Frolov S.M.ORCID,Zangiev A.E.,Zvegintsev V.I.ORCID,Shamshin I.O.ORCID

Funder

Ministry of Science and Higher Education of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference63 articles.

1. To the question of energy use of detonation combustion;Zel'dovich;Sov. J. Tech. Phys.,1940

2. Stationary spin detonation;Voitsekhovskii;Sov. J. Appl. Mech. Tech. Phys.,1960

3. Feasibility studies of a rotating detonation wave rocket motor;Nicholls;J. Spacecr. Rockets,1966

4. Continuous spin detonations;Bykovskii;J. Propuls. Power,2006

5. Numerical investigation of the physics of rotating-detonation engines;Schwer;Proc. Combust. Inst.,2011

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