Effect of the reaction mechanism on the numerical prediction of the performance of a scramjet combustor at cruise flight 8 Mach number-Reference-Cited by-同舟云学术

Effect of the reaction mechanism on the numerical prediction of the performance of a scramjet combustor at cruise flight 8 Mach number

Published:2021-05 Issue: Volume:112 Page:106595
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Rabadan Santana Edder^ORCID,Weigand Bernhard

Funder

German Research Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference62 articles.

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4. Investigation of hydrogen-air reaction mechanisms for supersonic combustion;Gerlinger,2008

5. Raman measurements of mixing and finite-rate chemistry in a supersonic hydrogen-air diffusion flame;Cheng;Combust. Flame,1994

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