Basic Design Philosophy and Systems: A Description of the Basic Requirements Leading to the Design of This Short-Haul, Twin Turbofan-Powered, Airliner Including Details of the Electrical, Hydraulic, Flying Control, Fuel, Air Conditioning, Pressurization, Anti-Icing, Oxygen and Fire Protection Systems and Associated Equipment

Author: A.F.I.A.S. A.J.K. Carline   F.R.Ae.S.  

Publisher: Emerald Group Publishing Ltd

ISSN: 0002-2667

Source: Aircraft Engineering, Vol.35, Iss.5, 1993-12, pp. : 127-141

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content