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The lift/drag coefficient of an Antonov An 225 is 19 with no change in the aerodynamics,Mach 4 mark,cruising altitude with the nett thrust payload of max.600 tonnes.
Um more like 4.273 which is the inverse of the Thrust. Max load 200 ton, and a service ceiling of 11,000m
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∙ 13y ago
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What is the world largest cammericial air craft?
The largest aircraft is the Antonov an225 the largest aircraft that is used to transport passengers is the Airbus A380
The biggest 10 planes in the world?
10}Boeing 737-300 9}Boeing 737-400 8}Boeing 737-500 7}Boeing 737-600 6}Airbus A360 5}Airbus A370 4}Airbus A380 3}Antonov An22 2}Antonov An225 1}Antonov An22
Relationship between coefficient lift and coefficient drag?
For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.
What is the zero lift drag coefficient of Airbus A330-200?
coefficient of drag in 0 lift
Is the c5a galexy the same as the an225?
NO
What is the lift coefficient of a f-117?
0.08
What is the coefficient of lift of a F-16?
0.016
What is the biggest plane in the world?
The Antonv An225
What is the maximum lift coefficient of a NACA-4412?
Yes
What is the lift coefficient of a cylinder?
It depends on the Reduced Velocity and amplitude of oscillation. Lift Coefficient could be as high as 1.0, and as low as -10.0 at very low reduced velocities.
Who invented antonov 225?
antonov airlines
What is the zero lift drag coefficient of airbus A380?
0.032
