Aerodynamics of a half-wing in supersonic flow

• Autorzy: Svirschevsky S. , Semenchikov N. , Tarkhow E. , Chernov G.
• Konferencja: Proceedings of the Third Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(III; 23-25.11.1998; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

Experimental results of the aerodynamic normal forces and moments of the semispan wing models are presented. All tests have been conducted at free stream Mach numbers M[infinity] = 1,5... 2,5, the angles of attack alpha= -4o ... 26° and the angles of sideslip beta= 0°...20°. Mounting effects on the model aerodynamic properties are considered. The test results of the semispan models can be used for a prediction of aerodynamic properties of sideslipping half-wings in a supersonic flow.

Słowa kluczowe

EN

aerodynamics; finite lenght; supersonic flow; experimental technology

• 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: 1999
• Tom: nr 9
• Strony: 135--138
• Opis fizyczny: Bibliogr. 4 poz., rys., wykr.

Twórcy

autor

Svirschevsky S.

autor

Semenchikov N.

autor

Tarkhow E.

autor

Chernov G.

• Moscow State Aviation Institute - Technical University, Russia