Planar 2D velocity measurements in the cap shock pattern of a thrust optimized rocket nozzle-Reference-Cited by-同舟云学术

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Planar 2D velocity measurements in the cap shock pattern of a thrust optimized rocket nozzle

Published:2011-10-13 Issue:1 Volume:22 Page:39-46
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Ramsey M. C.,Pitz R. W.,Jenkins T. P.,Matsutomi Y.,Yoon C.,Anderson W. E.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s00193-011-0340-0.pdf

Reference35 articles.

1. Hagemann G., Frey M., Koschel W.: Appearance of restricted shock separation in rocket nozzles. J. Propuls. Power 18(3), 577–584 (2002)

2. Hagemann G., Frey M.: Shock pattern in the plume of rocket nozzles: needs for design consideration. Shock Waves 17(6), 387–395 (2008). doi: 10.1007/s00193-008-0129-y

3. Frey M., Hagemann G.: Restricted shock separation in rocket nozzles. J. Propuls. Power 16(3), 478–484 (2000)

4. Wang T.S., Guidos M.: Transient three-dimensional side-load analysis of a film-cooled nozzle. J. Propuls. Power 25(6), 1272–1280 (2009). doi: 10.2514/1.41025

5. Wang T.S.: Transient three-dimensional startup side load analysis of a regeneratively cooled nozzle. Shock Waves 19(3), 251–264 (2009). doi: 10.1007/s00193-009-0201-2

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