A388NWO- wing, engines, empennage only.xlsx

	B	C	D	E	F	H	I	J	K	L	M	N	O	P	Q	R	S	T	U	V	X	Y	Z	AA	AB	AC	AD	AE	AF	AG	AH	AK	AL	AM
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8																											Thrust=
9				Pax	Cargo-	Cargo/		Cargo	Cargo					Wing					Air	Form/							Total				Misc	Weighted
10				Load	Equiv	Pax	Misc.	Load	Capac	Cargo	lbs	End	Start	Area		Wing	Wing	Wetted	Density	Roughness		Di	Dp	Di	Dp	Wave	Drag			TSFC	Drag	Fuel	Trip	Per Pax
11		MOEW	Pax	Factr	Pax	ratio	Items	Factr	Factr	Density	Cargo	Weight	Weight	FT2	AR	Span	loading	Area M2	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D	Facto	Delta	Burn	Ratio	Ratio
12	A380CEO	616,000	534	1.00	534	1,100	6,000	0.00	1.00	11.85	0	746,350	753,814	9106	7.77	266	82.78	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.50	0.50	0.040	1.00	1.00	1.000	1.00	0.00	1.00	1	1
13	A380NWO	480,000	534	1.00	534	1,100	6,000	0.00	1.00	11.85	0	605,304	609,961	7600	11.84	300	80.26	3,239.00	0.9695	0.980	3,174	0.52	0.885	0.26	0.44	0.032	0.70	0.81	1.157	0.89	0.00	0.62	0.624	0.6240
14											0	48	0.010						1.0000	0.996				0
15											0	15
16									Payload---->		120,150								Air	Cdp							Total
17												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
18		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
19	A380CEO	616,000	534		534						0	753,814	776,428	9106	7.77	266	85.27	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
20	A380NWO	480,000	534		534						0	609,961	623,555	7600	11.84	300	82.05	3,239.00	0.9622	0.980	3,065	0.53	0.855	0.29	0.34	0.040	0.68	0.81	1.198	0.89	0.00	0.60	0.607	0.6068
21								Segment A380CEO weight increment----->					0.030						0.9656	0.996				0
22
23																			Air	Cdp							Total
24												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
25		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
26	A380CEO	616,000	534		534						0	776,428	799,721	9106	7.77	266	87.82	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
27	A380NWO	480,000	534		534						0	623,555	637,451	7600	11.84	300	83.88	3,239.00	0.9550	0.980	3,042	0.53	0.848	0.29	0.34	0.040	0.67	0.80	1.198	0.89	0.00	0.60	0.602	0.6023
28													0						0.9584	0.996				0
29
30																			Air	Cdp							Total
31												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
32		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
33	A380CEO	616,000	534		534						0	799,721	823,712	9106	7.77	266	90.46	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
34	A380NWO	480,000	534		534						0	637,451	651,657	7600	11.84	300	85.74	3,239.00	0.9479	0.980	3,019	0.53	0.842	0.29	0.34	0.040	0.67	0.80	1.198	0.89	0.00	0.59	0.599	0.5992
35													0						0.9512	0.996				0
36
37																			Air	Cdp							Total
38												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
39		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
40	A380CEO	616,000	534		534						0	823,712	848,424	9106	7.77	266	93.17	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
41	A380NWO	480,000	534		534						0	651,657	666,180	7600	11.84	300	87.66	3,239.00	0.9408	0.980	2,997	0.52	0.836	0.29	0.33	0.039	0.66	0.79	1.198	0.89	0.00	0.59	0.596	0.5964
42													0						0.9441	0.996				0
43
44																			Air	Cdp							Total
45												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
46		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
47	A380CEO	616,000	534		534							848,424	873,876	9106	7.77	266	95.97	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
48	A380NWO	480,000	534		534							666,180	681,026	7600	11.84	300	89.61	3,239.00	0.9337	0.980	2,974	0.52	0.829	0.28	0.33	0.039	0.66	0.79	1.198	0.89	0.00	0.58	0.594	0.5938
49													0						0.9370	0.996				0
50
51																			Air	Cdp							Total
52												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
53		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
54	A380CEO	616,000	534		534							873,876	900,093	9106	7.77	266	98.85	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
55	A380NWO	480,000	534		534							681,026	696,203	7600	11.84	300	91.61	3,239.00	0.9268	0.980	2,952	0.51	0.823	0.28	0.33	0.039	0.65	0.78	1.198	0.89	0.00	0.58	0.591	0.5912
56													0						0.9300	0.996				0
57
58																			Air	Cdp							Total
59												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
60		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
61	A380CEO	616,000	534		534							900,093	927,096	9106	7.77	266	101.81	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
62	A380NWO	480,000	534		534							696,203	711,718	7600	11.84	300	93.65	3,239.00	0.9198	0.980	2,930	0.51	0.817	0.28	0.33	0.039	0.65	0.77	1.198	0.89	0.00	0.57	0.587	0.5872
63													0						0.9230	0.996				0
64
65																			Air	Cdp							Total
66												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
67		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
68	A380CEO	616,000	534		534							927,096	954,908	9106	7.77	266	104.87	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
69	A380NWO	480,000	534		534							711,718	727,579	7600	11.84	300	95.73	3,239.00	0.9129	0.980	2,908	0.51	0.811	0.28	0.32	0.038	0.64	0.77	1.198	0.89	0.00	0.57	0.583	0.5828
70													0						0.9161	0.996				0
71
72																			Air	Cdp							Total
73												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
74		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
75	A380CEO	616,000	534		534							954,908	983,556	9106	7.77	266	108.01	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
76	A380NWO	480,000	534		534							727,579	743,794	7600	11.84	300	97.87	3,239.00	0.9061	0.980	2,886	0.50	0.805	0.28	0.32	0.038	0.64	0.76	1.198	0.89	0.00	0.57	0.578	0.5785
77													0						0.9093	0.996				0
78
79																			Air	Cdp							Total
80												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
81		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
82	A380CEO	616,000	534		534							983,556	1,013,062	9106	7.77	266	111.25	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
83	A380NWO	480,000	534		534							743,794	760,370	7600	11.84	300	100.05	3,239.00	0.8993	0.980	2,865	0.50	0.799	0.27	0.32	0.038	0.63	0.76	1.198	0.89	0.00	0.56	0.574	0.5741
84													0						0.9025	0.996				0
85
86																			Air	Cdp							Total
87												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
88		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
89	A380CEO	616,000	534		534							1,013,062	1,043,454	9106	7.77	266	114.59	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
90	A380NWO	480,000	534		534							760,370	777,315	7600	11.84	300	102.28	3,239.00	0.8926	0.980	2,843	0.49	0.793	0.27	0.32	0.037	0.63	0.75	1.198	0.89	0.00	0.56	0.570	0.5698
91													0						0.8957	0.996				0
92
93																			Air	Cdp							Total
94												End	Start	Wing				Wetted	Density	Form		Di	Dp	Di	Dp	Wave	Drag					Fuel	Trip	Per Pax
95		MOEW	Pax									Weight	Weight	Area (S)	AR			Area	Ratio	Factor	Dp	Ratio	Ratio	Fraction	Fraction	Drag	Ratio	Lift	L/D			Burn	Ratio	Ratio
96	A380CEO	616,000	534		534							1,043,454	1,074,758	9106	7.77	266	118.03	3,586.00	1.0000	1.000	3,586	1.00	1.000	0.55	0.40	0.050	1.00	1.00	1.000	1.00	0.00	1.00	1.000	1.0000
97	A380NWO	480,000	534		534							777,315	794,638	7600	11.84	300	104.56	3,239.00	0.8859	0.980	2,822	0.49	0.787	0.27	0.31	0.037	0.62	0.74	1.198	0.89	0.00	0.55	0.566	0.5656
98													0						0.8890	0.996				0
99
100																			Air	Cdp							Total