Selection and Optimization of Aviation Gasious and Condensed Fuels by Criteria of Aircraft Efficiency

Aerospace propulsion engineering


Аuthors

Lukovnikov A. V.1*, Raznoschikov V. V.2, Yanovskaya M. L.3

1. Central Institute of Aviation Motors named after P.I. Baranov, CIAM, 2, Aviamotornaya str., Moscow, 111116, Russia
2. Zhukovsky Air Force Engineering Academy, 3, Planetnaya str., Moscow, 125190, Russia
3. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: Lukovnikof@mail.ru

Abstract

There are presented the concept and techniques and global mathematical model offered for estimation of new aviation fuel, optimized on structure, by criteria of a system efficiency «Aircraft – Engine – Fuel». Results of parameters optimization for turbojet operation process and structure aviation condensed gas fuel for subsonic transport aircraft of various load-carrying capacity are presented.

Keywords:

Engine; aircraft; aviation fuels; efficiency; optimization; mathematical modeling


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