Examples of 'lift coefficient' in a sentence
Meaning of "lift coefficient"
The lift coefficient is a dimensionless value that represents the effectiveness of an airfoil in generating lift. It is a measure of the aerodynamic performance of the airfoil, typically used in aviation and aerospace engineering
How to use "lift coefficient" in a sentence
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lift coefficient
The maximum lift coefficient is also increased.
Is determined to give the desired lift coefficient.
The dependence of the lift coefficient on the angle of attack.
Expect the separation to start at a lower lift coefficient.
Static lift coefficient.
Require a lower angle of attack to maintain the same lift coefficient.
This maximum lift coefficient will be largely insensitive to roughness effects.
Look at a profile curve of your wind turbine blade to determine the lift coefficient.
An alert lift coefficient is identified using the alert angle of attack.
It is also useful to show the relationship between section lift coefficient and drag coefficient.
A decrease in the lift coefficient indicates occurrence of stall at the rotor blade.
CL is also called your lift coefficient.
It is seen that the lift coefficient is very low for the transition region.
Subsequently, between medium and large angles of attack, the lift coefficient typically decreases.
Flaps raise the maximum lift coefficient of the aircraft and therefore reduce its stalling speed.
See also
These ranges enable a maximum value of the lift coefficient Cz to be obtained.
The lift coefficient is increased significantly for the governing inflow angles for the blade section.
Stall typically reduces the lift coefficient of the rotor blade significantly.
The lift coefficient depends on Reynolds number as shown in the tables and polar diagrams.
The results demonstrate that the lift coefficient increases when the flap and slat are deployed.
Lift coefficient Drag coefficient Pitching moment coefficient.
With respect to the necessary lift coefficient in order to obtain the correct axial induction.
Fig . 9 is a chart showing GAEP for different airfoil design lift coefficient and blade stations.
This maximum lift coefficient point corresponds to the critical AOA.
These ranges enable a minimum value of the lift coefficient Cz to be obtained.
The lift coefficient of a fixed-wing aircraft varies with angle of attack.
Angle of attack Lift coefficient cl.
The lift coefficient 61 increases until a maximum is reached.
By utilising a spoiler element, the maximum lift coefficient is increased significantly.
Figure 1, Lift coefficient improvement by vortex generator.
In general, it is desired to have a high lift coefficient and a low drag coefficient.
The maximum lift coefficient, CL, max, corresponds to the lift coefficient at astall.
Moreover, the maximum value of the lift coefficient c1 increases accordingly.
Even Wright brothers tested over 50 models to establish new lift coefficient.
It can be seen that the lift coefficient is increased significantly within the design AOA.
The method according to claim 20, wherein the method reduces a lift coefficient of the vehicle.
Consequently, the lift coefficient becomes larger.
A Gurney Flap smaller that 0.5 % yield only a small increase in lift coefficient CL.
Consequently, the lift coefficient becomes lower.
Czδq, lift coefficient of the tailplane ;.
A fixed leading-edge slot can increase the maximum lift coefficient of an airfoil section by 40.
Cl is the lift coefficient of the hydro foil 1 ;.
The lift / drag ratio is determined by dividing the lift coefficient by the drag coefficient, CI / CD.
In Figure 4, the lift coefficient CL is plotted as a function of the angle of attack, a.
At the same time, the maximum lift coefficient is found at a slightly lower inflow angle.
S The maximum lift coefficient ( CLmax ) achieved was approximately 0.26 lower than expected for the natural stall.
Line 1206 corresponds to the stall lift coefficient for an aircraft with respect to a Mach number.
FIG . 1, Lift coefficient improvement by vortex generator.
A jet flap effect increases the lift coefficient of the blade 17, thus increasing a lift / drag ratio.
The maximum lift coefficient was reduced from 1.8 clean.
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