Numerical Optimisation in Non Reacting Conditions of the Injector Geometry for a Continuous Detonation Wave Rocket Engine-Reference-Cited by-同舟云学术

Numerical Optimisation in Non Reacting Conditions of the Injector Geometry for a Continuous Detonation Wave Rocket Engine

Published:2015-06 Issue: Volume:111 Page:334-344
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gaillard T.^ORCID,Davidenko D.,Dupoirieux F.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

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2. Thermodynamic cycle analysis for propagating detonations;Wintenberger;Journal of propulsion and power,2006

3. J. A. Nicholls, R. E. Cullen, The feasibility of a rotating detonation wave rocket motor, Tech. rep., University of Michigan, RPL-TDR-64-113 (1964).

4. Performance analysis of a rotating detonation wave rocket engine;Adamson;Acta Astronautica,1967

5. Continuous spin detonations;Bykovskii;Journal of Propulsion and Power,2006

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