Influence of a heterogeneous combustion system in near wake of bodies of revolution on its drag force in supersonic flow

• Autorzy: Glagolev A. , Zubkov A. , Suhanovskaya L.
• 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

We had used non-conventional methods for heat and mass transfer determination to axisymmetric bodies in the base pressure and drag force control. The experiments were conducted in supersonic flow for Mach numbers within the range 1.15

Słowa kluczowe

EN

aerodynamics; combustion system; supersonic flow

PL

aerodynamika; system spalania; przepływ naddźwiękowy

• 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 11
• Strony: 81--86
• Opis fizyczny: Bibliogr. 11 poz., rys., tab., wykr.

Twórcy

autor

Glagolev A.

autor

Zubkov A.

autor

Suhanovskaya L.

• Institute of Mechanics, Moscow State University