Ridhima kapoor
November 1, 2016
8,923 views 59 plays
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A delta wing has
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The Lift/Drag ratio of a wing at the stalling angle is
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The airflow over the upper surface of a cambered wing
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The speed of air over a swept wing which contributes to the lift is
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In straight and level flight, the angle of attack of a swept wing is
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Induced drag
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A delta wing aircraft flying at the same speed (subsonic) and angle of attack as a swept wing aircraft of similar wing area will produce
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The stagnation point is
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If a swept wing stalls at the tips first, the aircraft will
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The thickness/chord ratio of the wing is also known as
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BO
this is more informative for me though. This helps me a lot of my exams and Ive passed it.
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January 12, 2021
Fahim Shaikh
Question 10 aspect ratio is ratio of wingspan to chord... answer is wrong.
March 9, 2021