lift curve

It is relatively simple to configure such systems to achieve the necessary control over the valve lift curve.

The lifted curve of their left hands, to show their certainty of agreement.

Because of the above-mentioned changes in lift curve slope, roll damping, as an example, is affected.

Figure 2 illustrates the different shape of the lift curves for leading edge and trailing edge stalls.

The lift drops for a very short time period before the usually assumed monotonically increasing lift curve is reached.

Ignacio found him dripping with water, sitting with his back to a palm trunk and staring out toward the lifting curve of the sea.

The lift curve is also influenced by the wing shape, including its airfoil section and wing planform.

With increased angle of attack, lift increases in a roughly linear relation, called the slope of the lift curve.

Full lift, drag and moment coefficient polars are produced, along with lift curve slope and natural trip locations.

The subtraction of two lift curves forms the uplift curve, which is a metric used in uplift modelling.

Integration of the jerk curve produces a smooth acceleration curve while the third integral gives an essentially ideal lift curve (cam profile).

C - Lift Curve Slope (Derivative of Lift Coefficient with respect to angle of attack)

Furthermore, decreasing the nacelle inclination led to higher lift curve slope values, which indicated that the powered wing could sustain higher angles of attack near maximum lift performance.

The lift curve can also be considered a variation on the receiver operating characteristic (ROC) curve, and is also known in econometrics as the Lorenz or power curve.

An Ehresmann connection also prescribes a manner for lifting curves from the base manifold M into the total space of the fibre bundle E so that the tangents to the curve are horizontal.

Originally Hall Royd Junction was triangular, and the lifted curve allowed services from Burnley to reach Manchester via Todmorden (regular services over it had ceased in November 1965).

Aspect ratio also affects the lift curve, a high aspect ratio wing will have a higher maximum CL but a lower stalling aoa than a low aspect ratio wing utilising the same aerofoil.

That increment is factored by the ratio of the wing to aerofoil lift curve slopes obtained respectively from ESDU 70011 and ESDU Aero W.01.01.05, thereby accounting for aspect ratio, taper and sweep effects.

In the case of the Spitfire, these forces acted on a very thin wing that was highly elastic, and in dives the wing would twist so much that the lift curve was opposed to the motion of the aileron, reversing the direction of the roll.