Numerical Modeling in Conjugate Formulation of the Temperature State of the Leading Edge of Hypersonic Flying Vehicles under Different Methods of Organization of the Cooling System

Author： Isaev S. A.   Leont'ev A. I.   Sadovnikov G. S.   Nosatov V. V.  

Publisher： Springer Publishing Company

ISSN： 1062-0125

Source： Journal of Engineering Physics and Thermophysics, Vol.76, Iss.5, 2003-09, pp. : 1043-1047

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