Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines-Reference-Cited by-同舟云学术

Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines

Published:2016 Issue:6 Volume:59 Page:332-339
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

KANDA Takeshi¹,SATO Masaki¹

Affiliation:

1. Research and Development Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/59/6/59_T-15-55/_pdf

Reference18 articles.

1. 1) Sutton, G. P. and Biblaz, O.: Rocket Propulsion Elements, 7th ed., John Wiley & Sons, 2000, pp. 285–286.

2. 2) Naraghi, M. H., Dunn, S., and Coats, D.: Modeling of Radiation Heat Transfer in Liquid Rocket Engines, AIAA Paper 2005-3935, 2005.

3. 3) Gobel, F., Kniesner, B., Frey, M., Knab, O., and Mundt, C.: Radiative Heat Transfer Analysis in Modern Rocket Combustion Chambers, Proceedings of 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, Jul. 2013.

4. 4) Schack, A.: Applied Heat Transfer, translated by Takahashi, Y., Corona, Co. Ltd., Tokyo, 1965, pp. 140–155, 278–279 (in Japanese).

5. 5) White, F. M.: Viscous Fluid Flow, McGraw-Hill, 1974, pp. 28–29, 31–32, 495, 632–644.

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