lift coefficient sentence in Hindi
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- 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.
- This means that a safety margin must be used on the main wing area so that its maximum lift coefficient and wing loading are never attained in practice.
- Where C _ L is the lift coefficient, " A " is the aspect ratio, and \ epsilon is the aircraft's efficiency factor.
- To achieve this stability, the change in canard lift coefficient with angle of attack ( lift coefficient slope ) should be less than that for the main plane.
- To achieve this stability, the change in canard lift coefficient with angle of attack ( lift coefficient slope ) should be less than that for the main plane.
- The lift coefficient with the wing at this setting was 3.9 ( double that of conventional and contemporary aircraft ), giving a stalling speed of 57 knots.
- Experiments have shown that it is not unreasonable to achieve a drag ratio ( \ gamma ) of about 0.01 at a lift coefficient of 0.6.
- Instead, the fuselage acts as a very large wing fence and, since wings are generally larger at the root, this raises the maximum lift coefficient allowing a smaller wing.
- The sections used were highly cambered in the leading edge with virtually no camber aft of mid chord, producing a section with reduced twisting and pitching moments and high lift coefficients.
- In aerodynamics, it is usual to use the top-view projected area of the wing, instead of its frontal area, as a reference surface to define the lift coefficient.
- When the wing is stalled and the angle of attack is greater than the stalling angle any increase in angle of attack causes a decrease in lift coefficient that causes the wing to descend.
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