Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels-Reference-Cited by-同舟云学术

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Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels

Published:2015-01 Issue: Volume:75 Page:600-607
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Pizzarelli Marco,Nasuti Francesco,Onofri Marcello,Roncioni Pietro,Votta Raffaele,Battista Francesco

Funder

Italian Ministry of University and Research

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference23 articles.

1. Experimental fatigue life investigation of cylindrical thrust chambers;Quentmeyer,1977

2. A thermal performance factor for evaluation of active engine cooling with asymmetric heating;Xu;Appl. Therm. Eng.,2014

3. History of Liquid Propellant Rocket Engines;Sutton,2006

4. A liquid propulsion panorama;Caisso;Acta Astronaut.,2009

5. Heat transfer and hydraulic resistance of supercritical-pressure coolants. part i: Specifics of thermophysical properties of supercritical pressure fluids and turbulent heat transfer under heating conditions in round tubes (state of the art);Kurganov;Int. J. Heat Mass Transf.,2012

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