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(i) A medium range airliner with the following design specification. Dimensions: Span 34.09 m Length 37.57 m Height 11.76 m Wing Area 122.6 m 2...
(i) A medium range airliner with the following design specification.
Dimensions:
Span 34.09 m
Length 37.57 m
Height 11.76 m
Wing Area 122.6 m2
Payload: Flight crew of two, maximum passenger accommodation in a high density layout of 179 passengers.
Empty weight: 42,220 kg
Maximum takeoff weight: 73,500 kg
Range: 150 passengers and reserves with CFM56s 4843km (2615nm), OR 5639km (3045nm), OR 5278km (2850nm); with V2500s 4874km (2632nm) OR optionally 5463km (2950nm) OR 5676km (3065nm)
Service ceiling: 12,000 m
System Design: Individual task (10%)
Instructions and guidelines:
· Each student in the group must prepare conceptual design of a system such as airframe, engine control system, flight control, electronics, navigation and communication, fuel system, environmental system, weapon system
