Numerical investigation of effects of cooling structure parameters on performance of flameholder in an integrated afterburner-Reference-Cited by-同舟云学术

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Numerical investigation of effects of cooling structure parameters on performance of flameholder in an integrated afterburner

Published:2022-02 Issue: Volume:121 Page:107378
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Jia Xiang-zhong^ORCID,Shan Yong^ORCID,Tan Xiao-ming^ORCID,Zhang Jing-zhou

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Turbofan forced mixer/nozzle temperature and flow field modelling;Koutmos;Int. J. Heat Mass Transf.,1989

2. GAS TURBINE COMBUSTION—alternative fuels and emissions;Lefebvre;J. Eng. Gas Turbines Power,2010

3. Unsteady simulations of turbulent flow behind a triangular bluff body;Madabhushi,1997

4. R. Madabhushi, D. Choi, T. Barber, Unsteady simulations of turbulent flow behind a triangular bluff body, 2015.

5. T.R. Clements, C.B. Graves, Augmentor burner, 1995.

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