Effective Modeling of Conjugate Heat Transfer and Hydraulics for the Regenerative Cooling Design of Kerosene Rocket Engines-Reference-Cited by-同舟云学术

Effective Modeling of Conjugate Heat Transfer and Hydraulics for the Regenerative Cooling Design of Kerosene Rocket Engines

Published:2014-06-25 Issue:8 Volume:66 Page:863-883
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Kim Seong-Ku,Joh Miok,Choi Hwan Seok,Park Tae Seon

Funder

The present work was carried out under the Research and Development of the Korea Space Launch Vehicle-II program sponsored by the Ministry of Science, ICT & Future Planning.

Publisher

Informa UK Limited

Subject

Condensed Matter Physics,Numerical Analysis

Link

http://www.tandfonline.com/doi/pdf/10.1080/10407782.2014.892396

Reference24 articles.

1. Y. Daimon , H. Negishi , N. Yamanishi , Y. Nunome , M. Sasaki , and T. Tomita , Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2012-4009, Atlanta, Georgia , 2012 .

2. Heat Transfer of Aviation Kerosene at Supercritical Conditions

3. M. H. Naraghi , S. Dunn , and D. Coats , A Model for Design and Analysis of Regeneratively Cooled Rocket Engines, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2004-3852, Fort Lauderdale, FL , 2004 .

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