Supersonic low interaction with absorbing surface

• Autorzy: Svirschevsky S. , Nikitchenko Y.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

This paper is devoted to investigation of shock wave rise conditions ahead of an absorbing surface. The study was based on the numerical solution of the model of kinetic equations BGK in an integral form. It was found that the boundary between the regions of steady, non-steady modes in one-dimensional problem corresponds to the boundary of the shock wave existence area for a multi-dimensional problem.

Słowa kluczowe

EN

supersonic flow; absorbing surface; shock wave

PL

przepływ supersoniczny; powierzchnia absorbująca; fala uderzeniowa

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2001
• Tom: nr 12
• Strony: 93--96
• Opis fizyczny: Bibliogr. 4 poz., rys., wykr.

Twórcy

autor

Svirschevsky S.

autor

Nikitchenko Y.

• Moscow State Aviation Institute - Technical University, Moscow, Russia