Consider an airfoil in a

Which of the statemets below about a thick airfoil is not true?A thick airfoil will have a higher (more positive) pressure
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Consider an airfoil in a flow of air, where far ahead (upstream) of the airfoil, the pressure, velocity and density are:1.01 10
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Consider an airfoil flying at M=0.7.What is the critical pressure coefficient for this airfoil?
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Consider an airfoil flying at 100 m/s under standard sea-level conditions. The airfoil has a very low thickness, so it can be
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You are given four statements about the NACA airfoil with code “XYZZ”:The X stands for the camber as percentage of the wing
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2. asked by shawon
3. 98 views
You are given four statements about the NACA airfoil with code “XYZZ”:The X stands for the camber as percentage of the wing
1. 1 answer
2. asked by shawon
3. 98 views
You are given four statements about the NACA airfoil with code “XYZZ”:The X stands for the camber as percentage of the wing
1. 1 answer
2. 29 views
Which of the following statements about airfoils and wings is/are true?An airfoil only feels two-dimensional flow, while a wing
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2. 32 views
Consider the following statements:1. When the airfoil is at conditions, separation takes place around 85-90% of the chord. 2.
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Why do we invert the (y) axis in the pressure distribution plot?Because the pressure spike is otherwise not clearly visible
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