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For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.
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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.
Is lift a synonym for elevate?
Lift is a synonym for elevate
What does exalting mean?
the most high the most great
Which one is stronger a boy or a girl?
It actually depends if they lift weights or not. So, it could be either one of them.
How much is done if you exert a 25-N force to lift a ball 0.4 m in 2 s?
10 J (novanet)
What is the zero lift drag coefficient of Airbus A330-200?
coefficient of drag in 0 lift
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 is the relationship of lift drag thrust and weight when the airplane is in straight-and-level flight?
Lift equals weight and thrust equals drag.
What is the relationship between the 4 forces of flight?
Lift is opposite of weight Thrust is opposite drag. When lift >weight plane climbs. If lift < weight you best find a place to land. If thrust> drag you accelerate. If drag>thrust you slow down. High and fast are your friends. Low and slow are out to kill you.
What is the dfference between lift and drag?
drag you pull across the ground lift you pick up and take around
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
Is there relationship between lift and weight?
yes there is
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 much lift will a wing generate?
A wing will generate lift according to the following equation: L = ½ A C ρ v² A = wing area C = lift coefficient ρ = air density v = air speed The lift coefficient C is a function of Angle of Attack (AOA), which is the angle between the wing's chord line and the relative wind. The greater the angle, the greater the lift coefficient up until the critical AOA where the wing begins to stall and lose lift. The lift coefficient is also a function of wing aspect ratio and will be specific to a certain airfoil shape.
How are the lift and drag components of the wing affected when you lower the flaps?
lift decrease and increase drag
