Numerical investigations of different liner lengths of axial film cooling for a rotating detonation engine-Reference-Cited by-同舟云学术

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Numerical investigations of different liner lengths of axial film cooling for a rotating detonation engine

Published:2024-06 Issue: Volume:149 Page:109172
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Lv Haiyin,Xu Jinglei^ORCID,Li Rui,Zhou Junfei,Yu Kaikai

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference53 articles.

1. Overview of performance, application, and analysis of rotating detonation engine technologies;Rankin;J. Propuls. Power,2017

2. Determining the pressure gain of pressure gain combustion;Kaemming,2018

3. A review of aircraft subsonic and supersonic combustors;Abdulrahman;Aerosp. Sci. Technol.,2022

4. Progress of continuously rotating detonation engines;Zhou;Chin. J. Aeronaut.,2016

5. Impulse response processing of transient heat transfer gauge signals;Oldfield;J. Turbomach.,2008

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