Experimental and numerical investigation of ethanol film cooling

Author:

Soller SebastianORCID,Riedmann Hendrik,Simonini Alessia,Gouriet Jean-Baptiste,Strauss Friedolin,Kirchberger Christoph,Dinescu Cristian,Claramunt Kilian,Steelant Johan

Funder

European Space Agency

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference18 articles.

1. Kinney, G.R., Abramson, J.L.: Internal-liquid-film-cooling experiments with air stream temperatures to 2000°f in 2- and 4-inch-diameter horizontal tubes. US Government Printing Office, Washington (1952)

2. Abramson, A. E.: Investigation of internal film cooling of exhaust nozzle of a 1000-pound liquid-ammonia liquid-oxygen rocket, NACA Research Memorandum NACA RM E52C26, National Advisory Committee for Aeronautics, Washington (1952)

3. Morrell, G.: Investigation of internal film cooling of 1000-pound liquid-ammonia liquid-oxygen rocket engine combustion chamber, NACA Research Memorandum NACA RM E51E04, National Advisory Committee for Aeronautics, Washington (1951)

4. Yu, Y., Schuff, R., W.: Anderson: Liquid Film cooling using swirl in rocket combustors, AIAA 2004-3360, 4oth AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Luderdale, Florida. (2004)

5. Kinney, G.R., Abramson, J.L., Sloop, J.L.: Internal-liquid-film-cooling experiments with air stream temperatures to 2000°f in 2- and 4-inch-diameter horizontal tubes. US Government Printing Office, Washington (1952)

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