Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference-Reference-Cited by-同舟云学术

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Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference

Published:2018-02 Issue: Volume:130 Page:1598-1609
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Cheng Kunlin,Qin Jiang,Jiang Yuguang,Lv Chuanwen,Zhang Silong,Bao Wen

Funder

Innovative Research Groups

National Natural Science Foundation of China

Shenzhen Technology Projects

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference48 articles.

1. Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle;Bolender;J. Spacecr Rockets,2007

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

3. Oxidation-resistant high-temperature materials;Newman;Johns Hopkins APL Tech. Dig.,1993

4. Quasi-one-dimensional model of scramjet combustor coupled with regenerative cooling;Zhang;J. Propuls Power,2016

5. Cooling, heating, generating power, and recovering waste heat with thermoelectric systems;Bell;Science,2008

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