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

Table 3

Data collection for wide-body transport aircraft.

List of aircraft	Decision criteria
	C1	C2	C3	C4	C5	C6	C7	C8	C9	C10	C11	C12	C13
	Aerodynamic consideration		Structural consideration				Performance and operational consideration					Economic consideration
	FR	AR	MTOW (kg)			nPL	(kg/m^2)		R (km)	STO (m)	(km/h)	ROC (m/s)	SFC (kg/hr/N)
A1	9.45	7.7	170500	0.52	0.316	375	655.77	0.307	7500	2280	897	16.26	0.0125
A2	8.27	8.8	144000	0.551	0.333	275	655.77	0.307	6500	2280	850	15.24	0.0122
A3	12.1	8.5	227703	0.551	0.701	460	657.53	0.307	1333	2280	1005	15.24	0.0186
A4	11.1	9.3	217000	0.544	0.357	440	597.63	0.281	11760	2770	870	10.16	0.0096
A5	11.1	9.3	271000	0.479	0.413	440	746.35	0.227	13700	3000	913	28.96	0.0123
A6	12.3	8.5	365000	0.485	0.423	475	834.67	0.278	14600	3140	915	28.96	0.0097
A7	10.2	7.5	575000	0.482	0.442	853	680.47	0.246	15400	3000	1099	7.62	0.013
A8	11.9	9.5	280000	0.413	0.394	440	633.48	0.273	15000	2600	945	7.62	0.0093
A9	12.1	9.0	286670	0.491	0.385	480	633.48	0.273	16100	2600	945	15.24	0.0075
A10	10.5	6.9	340195	0.497	0.461	516	665.74	0.250	9800	3246	939	5.08	0.018
A11	10.5	6.9	377840	0.465	0.427	516	739.43	0.254	12700	3200	969	5.08	0.013
A12	10.5	7.3	396830	0.457	0.407	660	755.87	0.259	13450	3310	933	7.62	0.0111
A13	10.1	8.6	286897	0.481	0.466	440	670.64	0.265	14000	2438	950	15.24	0.0121
A14	11.8	8.7	299370	0.521	0.452	550	699.78	0.288	11165	3230	950	15.24	0.0136
A15	11.8	9.6	254011	0.533	0.399	440	673.7	0.273	11750	2800	954	15.24	0.0121
A16	12.4	9.9	352441	0.511	0.451	426	682.1	0.270	20372	3000	1034	15.24	0.0086
A17	8.6	6.9	263636	0.461	0.414	380	716.99	0.273	9630	3000	981	10.16	0.0157
A18	9.7	7.9	283720	0.473	0.424	405	837.18	0.295	13408	3139	961	10.16	0.0105
A19	8.9	6.9	211374	0.529	0.374	400	657.46	0.270	6667	2350	957	14.224	0.0202
A20	9.23	7.2	208000	0.4	0.4324	350	650	0.249	10000	2700	869	15	0.0153
A21	8.41	7.89	216000	0.542	0.551	300	650	0.249	11500	2400	850	15	0.014
A22	9.95	7.89	270000	0.49	0.44	375	650	0.249	10000	2600	870	15	0.0157