Heat transfer on secondary injection surface with backward-facing step influenced by hole location in supersonic flow field-Reference-Cited by-同舟云学术

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Heat transfer on secondary injection surface with backward-facing step influenced by hole location in supersonic flow field

Published:2024-09 Issue: Volume:157 Page:107816
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Bae Hyung Mo,Kim Jihyuk,Nam Juyeong,Lee Namkyu,Cho Hyung Hee

Publisher

Elsevier BV

Reference31 articles.

1. Fluid phenomena in scramjet combustion systems;Curran;Annu. Rev. Fluid Mech.,1996

2. Scramjet Combustion: Fundamentals and Advances;Choubey,2022

3. Recent research progress on transverse injection technique for scramjet applications-a brief review;Choubey;Int. J. Hydrog. Energy,2020

4. Study on main flow and fuel injector configurations for scramjet applications;Ali;Int. J. Heat Mass Transf.,2006

5. Scramjets: Fuel Mixing and Injection Systems;Gerdroodbary,2020

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