A new generalised model for liquid film cooling in rocket combustion chambers-Reference-Cited by-同舟云学术

A new generalised model for liquid film cooling in rocket combustion chambers

Published:2012-09 Issue:19-20 Volume:55 Page:5065-5075
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Shine S.R.,Sunil Kumar S.,Suresh B.N.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference41 articles.

1. Selecting cooling techniques for liquid rockets for spacecraft;Coulbert;J. Spacecraft Rockets,1964

2. E.L. Knuth, The mechanism of film cooling, Ph.D. thesis, California Institute of Technology, 1954.

3. An approximate theory of porous, sweat, or film cooling with reactive fluids;Crooco;J. Am. Rocket Soc.,1952

4. D.L.Emmons, Effects of selected gas stream parameters and coolant physical properties on film cooling a rocket motor, Technical Report, Report No.TM-62-5, Purdue University, 1962.

5. Heat transfer in turbulent shear flow;Rannie;J. Aeronaut. Sci.,1956

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