Modern military aircraft engines

• Autorzy: Błaszczyk J. , Chachurski R. , Kozakiewicz A. , Zalewski P.
• 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

Propulsion systems of modem multirole aircraft are presented in the paper focusing on concept, requirements, state of the art. The requirements, imposed by the multi-role aircraft concept on their power plant are presented and discussed. This paper also highlights the problem of number of engines, survivability, etc. The turbofan engines of primary multirole aircraft both in service and at the development stage were compared and evaluated as well. Their essential parameters which have a direct impact on the aircraft performance: such as, specific thrust, thrust to weight ratio, specific fuel consumption, bypass ratio, mass and other were assessed. The comparison both contemporary engines and their parameters can reveal the development trends in military engine technology.

Słowa kluczowe

EN

modern military aircraft; engines; combat aircraft

PL

nowoczesne samoloty wojskowe; silniki; samoloty bojowe; samoloty odrzutowe

• 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: 2000
• Tom: nr 10
• Strony: 49--56
• Opis fizyczny: Bibliogr. 9 poz., rys., tab., wykr.

Twórcy

autor

Błaszczyk J.

autor

Chachurski R.

autor

Kozakiewicz A.

autor

Zalewski P.

• Military University of Technology, Warsaw, Poland