Heat transfer characteristics of a concentric annular high temperature heat pipe under anti-gravity conditions

Author:

Zhao Jie,Yuan Da-Zhong,Tang Da-Wei,Jiang Yu-Yan

Funder

National Nature Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference20 articles.

1. Heat pipe for aerospace applications—an overview;Shukla;J. Electron. Cool. Therm. Control,2015

2. Feasibility of metallic structural heat pipes as sharp leading edges for hypersonic vehicles;Steeves;J. Appl. Mech.,2009

3. C.J. Camarda, D.E. Glass, Thermo-structural applications of heat pipes for cooling leading edges of high-speed aerospace vehicles, NASA STI/Recon Technical Report N, 93 (1992) 291–318.

4. Second generation sodium heat pipe receiver for a USAB V-160 Stirling engine: evaluation of on-sun test results using the proposed IEA guidelines and analysis of heat pipe damage;Laing;J. Sol. Energy Eng.,1997

5. Hybrid dish/Stirling systems: combustor and heat pipe receiver development;Laing;J. Sol. Energy Eng.,2002

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