Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study-Reference-Cited by-同舟云学术

Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study

Published:2022-06-23 Issue: Volume: Page:1-22
ISSN:0891-6152
Container-title:Experimental Heat Transfer
language:en
Short-container-title:Experimental Heat Transfer

Author:

Zou Zhengping¹²,Wang Yifan²,Li Hui²,Chen Yiming¹²,Yao Lichao¹²,Li Huan²,Liu Huoxing¹²

Affiliation:

1. Research Institute of Aero-Engine Beihang University, Beijing, China

2. National Key Laboratory of Science and Technology on Aero-Engine Aerothermodynamics, School of Energy & Power Engineering, Beihang University, Beijing, China

Funder

Young Elite Scientists Sponsorship Program, CAST, China

Publisher

Informa UK Limited

Subject

Electrical and Electronic Engineering,Instrumentation,Control and Systems Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/08916152.2022.2086323

Reference49 articles.

1. Thermodynamic efficiency analysis and cycle optimization of deeply precooled combined cycle engine in the air-breathing mode

2. Precooler-design & engine-performance conjugated optimization for fuel direct precooled airbreathing propulsion

3. Research on hypersonic aircraft using pre-cooled turbojet engines

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