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单词 lift coefficient
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Examples oflift coefficient

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Theliftcoefficientis very sensitive to various numerical parameters.
From theCambridge English Corpus
The numerical results forliftcoefficientare summarized in figure 14.
From theCambridge English Corpus
The flow exhibits characteristic force pulsations with distinct regions of high and low values of the drag andliftcoefficient(see figure 2).
From theCambridge English Corpus
An expression for theliftcoefficientat small clearance and angle of attack, valid for moderate aspect ratio, is derived.
From theCambridge English Corpus
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.
From theCambridge English Corpus
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.
From theCambridge English Corpus
Forward-swept wings yield a higher maximumliftcoefficient, reduced bending moments, and delayed stall when compared to more traditional wing shapes.
From
Wikipedia
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The more elongated the sail, the less lift-induced drag alters value of theliftcoefficient.
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Together these high-lift devices produced a maximum wingliftcoefficientof 3.0 (based on the flap-retracted wing area).
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If the angle of attack and velocity remain constant, an increase in theliftcoefficientwill result, which accounts for the floating effect.
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Increasing angle of attack is associated with increasingliftcoefficientup to the maximumliftcoefficient, after whichliftcoefficientdecreases.
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In conjunction with a slat, the increase in maximumliftcoefficientcan be 50% or even 60%.
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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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It is also useful to show the relationship between sectionliftcoefficientand drag coefficient.
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For a symmetric airfoil, as angle of attack andliftcoefficientchange, the center of pressure does not move.
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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 model was more successful and resulted in the highest lift capacity, as measured by the maximumliftcoefficientrecorded up to that time.
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The benefit of the circulation control wing is that no extra drag is created and theliftcoefficientis greatly increased.
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As a result, the stall is delayed momentarily and aliftcoefficientsignificantly higher than the steady-state maximum is achieved.
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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.

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更新时间:2024/12/28 9:53:14