Performance assessment of a closed-recuperative-Brayton-cycle based integrated system for power generation and engine cooling of hypersonic vehicle-Reference-Cited by-同舟云学术

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Performance assessment of a closed-recuperative-Brayton-cycle based integrated system for power generation and engine cooling of hypersonic vehicle

Published:2019-04 Issue: Volume:87 Page:278-288
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cheng Kunlin,Qin Jiang,Sun Hongchuang,Dang Chaolei,Zhang Silong,Liu Xiaoyong,Bao Wen

Funder

National Natural Science Foundation of China

Shenzhen Technology Projects

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Control-oriented modeling of an air-breathing hypersonic vehicle;Parker;J. Guid. Control Dyn.,2007

2. Two-stage-to-orbit spaceplane concept with growth potential;Mehta;J. Propuls. Power,2001

3. Performance evaluation of power generation system with fuel vapor turbine onboard hydrocarbon fueled scramjets;Zhang;Energy,2014

4. Detailed design of a high speed switched reluctance starter/generator for more/all electric aircraft;Song;Chin. J. Aeronaut.,2010

5. Electric power generation onboard hypersonic aircraft;Sforza,2009

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