A simplified numerical method based on anisotropic porous media model for the precooler of the hypersonic precooled engine-Reference-Cited by-同舟云学术

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A simplified numerical method based on anisotropic porous media model for the precooler of the hypersonic precooled engine

Published:2024-09 Issue: Volume:252 Page:123709
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Wei Xin^ORCID,Shi Xiaojuan,Ji Honghu,Jin Feng

Publisher

Elsevier BV

Reference37 articles.

1. Developments in high-speed vehicle propulsion systems;Murthy;Prog. Astronaut. Aeronaut. AIAA,1996

2. Overview of the development of heat exchangers for use in air-breathing propulsion pre-coolers;Murray;Acta Astronaut.,1997

3. A comparison of propulsion concepts for SSTO reusable launchers;Varvill;J. Br. Interplanet. Soc.,2003

4. Study on multi-cycle coupling mechanism of hypersonic precooled combined cycle engine;Dong;Appl. Therm. Eng.,2018

5. Enhancement of performance of gas turbine engines by inlet air cooling and cogeneration system;Najjar;Appl. Therm. Eng.,1996

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