Investigation of conjugate circular arcs in rocket nozzle contour design
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/article/10.1007/s00193-018-0834-0/fulltext.html
Reference25 articles.
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2. Shapiro, A.: Nozzles for supersonic flow without shock fronts. J. Appl. Mech. 11(2), 93–100 (1944)
3. Ahlberg, J., Hamilton, S., Migdal, D., Nilson, E.: Truncated perfect nozzles in an optimum nozzle design. ARS J. 31(5), 614–620 (1961). https://doi.org/10.2514/8.5577
4. Gogish, L.: A study of short supersonic nozzles. Fluid Dyn. 1(2), 122–126 (1966). https://doi.org/10.1007/bf01013838
5. Watanabe, Y., Sakazume, N., Yonezawa, K., Tsujimoto, Y.: LE7A engine nozzle flow separation phenomena and a method of RSS suppression with a step inside nozzle. J. Jpn. Soc. Aeronaut. Space Sci. 55(645), 474–482 (2007). https://doi.org/10.2322/jjsass.55.474
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