Optimization of the rocket’s nose and nozzle design parameters in respect to its aerodynamic characteristics

A. Fedaravicius1 , S. Kilikevicius2 , A. Survila3

Journal of Vibroengineering, Vol. 14, Issue 4, 2012, p. 1885-1891.
Received 11 November 2012; accepted 4 December 2012; published 31 December 2012

Copyright © 2012 Vibroengineering This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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