Modelling and Design Optimization of a Novel Wide-Body Transport Aircraft to Improve the Structural Integrity

Table 5

Computed the rank of the WASPAS technique.

Alternative decision variables		λ = 0	λ = 0.5	λ = 1	Model aircraft
		Rank	Rank	Rank
Choose the baseline aircraft	A1	20	3	3	Airbus A300-600R
	A2	22	1	1	Airbus A310-200
	A3	5	18	18	Airbus A330-900N
	A4	16	8	8	Airbus A330-300
	A5	17	7	6	Airbus A340-300
	A6	15	6	7	Airbus A340-600
	A7	3	20	20	Airbus A380-800
	A8	18	5	5	Airbus A350-900
	A9	21	2	2	Airbus A350-1000
	A10	1	22	22	Boeing B747-100
	A11	2	21	21	Boeing B747-200
	A12	4	19	19	Boeing B747-400
	A13	14	9	9	Boeing B777-200IGW
	A14	6	17	17	Boeing B777-300
	A15	11	12	12	Boeing B787-dreamliner10
	A16	19	4	4	Boeing B777-9X
	A17	7	16	16	Doug. DC10-30
	A18	10	13	13	McDON./Doug. MD-11
	A19	9	14	14	Lock Hd L1011-100
	A20	12	11	11	Ilyushin Il-86
	A21	13	10	10	Ilyushin Il-96-300
	A22	8	15	15	Ilyushin Il-96M