Experimental investigation on convective heat transfer from a horizontal miniature tube to methane at supercritical pressures-Reference-Cited by-同舟云学术

Experimental investigation on convective heat transfer from a horizontal miniature tube to methane at supercritical pressures

Published:2013-09 Issue:1-2 Volume:58 Page:490-498
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Gu Hongfang,Li Hongzhi,Wang Haijun,Luo Yushan

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference21 articles.

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2. Effect of combustion process on performance, stability, and durability of a LOX/methane rocket engine;Craig Judd;AIAA J.,2006

3. Z. Stephan, J.L. Thomas, P. Vuillermoz, et al., Recent advances on LOX/methane combustion for liquid rocket engine injector, Indianapolis, United States, 2002.

4. Rocket Propulsion Elements;Sutton,2001

5. Heat transfer from supercritical carbon dioxide in tube flow: a critical review;Pitla;Int. J. Heat. Vent. Air Cond. Refrig. Res.,1998

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