lift coefficient उदाहरण वाक्य
उदाहरण वाक्य
- As the wing rises the angle of attack decreases and causes the lift coefficient to increase further towards the maximum lift coefficient.
- Ornithopters with thinner wings have a limited angle of attack but provide optimum minimum-drag performance for a single lift coefficient.
- In this case, the wing can be flown at higher lift coefficient ( closer to stall ) to produce more overall lift.
- Suction side surface cavitation forms when the propeller is operating at high rotational speeds or under heavy load ( high blade lift coefficient ).
- As the wing descends the angle of attack increases, which causes the lift coefficient to decrease and the angle of attack to increase.
- The wing may thus be used up to its maximum lift coefficient, an advantage that may translate into a reduction of its area and weight.
- Together, these high-lift devices produced a maximum wing lift coefficient of 3.0 ( based on the flap-retracted wing area ).
- The lift coefficient can be approximated using the lifting-line theory, numerically calculated or measured in a wind tunnel test of a complete aircraft configuration.
- The angle at which maximum lift coefficient occurs is the stall angle of the airfoil, which is approximately 10 to 15 degrees on a typical airfoil.
- Therefore, the most common way in which pitch stability can be achieved is to increase the lift coefficient ( so the wing loading ) of the canard.