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What is the zero lift drag coefficient of Airbus A330-200?
coefficient of drag in 0 lift
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 zero lift coefficient of drag?
For no lift, The induced drag will be zero. However, there will still be drag due to viscous forces and pressure forces.
What is the zero lift drag coefficient of airbus A380?
0.032
What does lift and stag mean in a rocket?
LIft = coefficient times density times velocity squared times wing area divided by 2 drag= coefficient times density times velocity squared over 2 times reference area
What is the lift coefficient of an Antonov An-225?
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
Why drag increases as lift increase - for helis?
The production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
How are the lift and drag components of the wing affected when you lower the flaps?
lift decrease and increase drag
What is the airspeed needed to lift off on a Cessna 172?
55-70Knots
How does the lift thrust drag and gravity affect a helicopter?
Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.
How does angle of attack affect lift and drag?
A higher angle of attack has an increase of both lift and drag.
What is the lift coefficient of a f-117?
0.08
