Simulation of reducing the drag of a Soyuz-type missile’s reentry vehicle with a coaxial disk placed in front of it.
Autor: | Isaev, S. A.1 isaev3612@yandex.ru, Lipnitskii, Yu. M.2, Mikhalev, A. N.3, Panasenko, A. V.2, Baranov, P. A.1 |
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Zdroj: | Technical Physics Letters. Aug2013, Vol. 39 Issue 8, p748-750. 3p. |
Databáze: | Academic Search Ultimate |
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