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Examples oflift coefficient
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Theliftcoefficientis very sensitive to various numerical parameters.
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The numerical results forliftcoefficientare summarized in figure 14.
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The flow exhibits characteristic force pulsations with distinct regions of high and low values of the drag andliftcoefficient(see figure 2).
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An expression for theliftcoefficientat small clearance and angle of attack, valid for moderate aspect ratio, is derived.
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The two-dimensional flat plate airfoil is examined in detail and results for upper and lower surface pressure distribution andliftcoefficientare compared with a numerical solution.
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Hence, a unit-orderliftcoefficientand an optimum lift/drag ratio in the range 5-10 are attainable even in the presence of massive flow separation in this case.
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Forward-swept wings yield a higher maximumliftcoefficient, reduced bending moments, and delayed stall when compared to more traditional wing shapes.
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This example is from Wikipedia and may be reused under a CC BY-SA license.The more elongated the sail, the less lift-induced drag alters value of theliftcoefficient.
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This example is from Wikipedia and may be reused under a CC BY-SA license.Together these high-lift devices produced a maximum wingliftcoefficientof 3.0 (based on the flap-retracted wing area).
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This example is from Wikipedia and may be reused under a CC BY-SA license.If the angle of attack and velocity remain constant, an increase in theliftcoefficientwill result, which accounts for the floating effect.
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This example is from Wikipedia and may be reused under a CC BY-SA license.Increasing angle of attack is associated with increasingliftcoefficientup to the maximumliftcoefficient, after whichliftcoefficientdecreases.
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This example is from Wikipedia and may be reused under a CC BY-SA license.In conjunction with a slat, the increase in maximumliftcoefficientcan be 50% or even 60%.
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This example is from Wikipedia and may be reused under a CC BY-SA license.As the wing descends, the angle of attack andliftcoefficientincrease which tends to restore the wing to its original angle of attack.
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This example is from Wikipedia and may be reused under a CC BY-SA license.It is also useful to show the relationship between sectionliftcoefficientand drag coefficient.
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This example is from Wikipedia and may be reused under a CC BY-SA license.For a symmetric airfoil, as angle of attack andliftcoefficientchange, the center of pressure does not move.
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This example is from Wikipedia and may be reused under a CC BY-SA license.Therefore, the most common way in which pitch stability can be achieved is to increase theliftcoefficient(so the wing loading) of the canard.
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This example is from Wikipedia and may be reused under a CC BY-SA license.This model was more successful and resulted in the highest lift capacity, as measured by the maximumliftcoefficientrecorded up to that time.
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This example is from Wikipedia and may be reused under a CC BY-SA license.The benefit of the circulation control wing is that no extra drag is created and theliftcoefficientis greatly increased.
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This example is from Wikipedia and may be reused under a CC BY-SA license.As a result, the stall is delayed momentarily and aliftcoefficientsignificantly higher than the steady-state maximum is achieved.
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This example is from Wikipedia and may be reused under a CC BY-SA license.These examples are from corpora and from sources on the web. Any opinions in the examples do not represent the opinion of the Cambridge Dictionary editors or of Cambridge University Press or its licensors.