Parameter.xlsx

	A	B	C
1	Parameters	Aircraft	Unit
2	Rolling Resistance Calculation
3	Kerb Weight	575000	kg
4	Total Weight	575000	kg
5	Coefficent of Rolling resitance	0.002	m/s^2
6	Acceleration due to gravity (G)	9.81	N
7	Rolling Resistance Force (Frr)	11281.5
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9	Air Drag Calcution
10	Air Density	1.125	kg/m^2
11	Width	10	m
12	Height	15	m^2
13	Frontal Area	150
14	Air Drag co-efficient Cd for Aircraft	0.025
15	Speed (V)	4	m/s
16	Air Drage Force(Fad)	33.75
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18	Hill climbing angle	0	Rad
19	Sine	0	Rad
20	Fhc	0
21	Total tractive force (Fte)	11315.25	N
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23	Power Reqired	45.261	kW
24
25	Duty cycle
26	Voltage	400	V
27	Peak Power	60	kW
28	RPM	1500-4000	rpm
29	Torque	300	Nm
30	Battery Power(Assumed)	550	V
31
32	Duty Cycle	0.75
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