Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines-Reference-Cited by-同舟云学术

Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines

Published:2018-06 Issue: Volume:147 Page:281-296
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Candon M.J.^ORCID,Ogawa H.

Funder

Australian Research Council through the DECRA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. X-43 – scramjet power breaks the hypersonic barrier dryden lectureship in research for 2006;McClinton,2006

2. X-51 Development: a Chief Engineer's Perspective, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;Mutzman,2011

3. The Standard Handbook for Aeronautical and Astronautical Engineers;Davies,2003

4. Observation of supersonic free shear layers;Papamoschou,1986

5. CFD analysis of mixing and combustion of a scramjet combustor with a planer strut injector;Pandey;Int. J. Env. Sci. and Dev.,2011

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