Consider again the airfoil of

Which of the statemets below about a thick airfoil is not true?A thick airfoil will have a higher (more positive) pressure
1. 1 answer
2. 36 views
Consider an airfoil in a flow of air, where far ahead (upstream) of the airfoil, the pressure, velocity and density are:1.01 10
1. 1 answer
2. 30 views
Consider an airfoil flying at M=0.7.What is the critical pressure coefficient for this airfoil?
1. 1 answer
2. 28 views
Consider an airfoil flying at 100 m/s under standard sea-level conditions. The airfoil has a very low thickness, so it can be
1. 1 answer
2. 37 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. 96 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. 96 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. 27 views
Which of the following statements about airfoils and wings is/are true?An airfoil only feels two-dimensional flow, while a wing
1. 1 answer
2. 31 views
Consider the following statements:1. When the airfoil is at conditions, separation takes place around 85-90% of the chord. 2.
1. 1 answer
2. 19 views
Why do we invert the (y) axis in the pressure distribution plot?Because the pressure spike is otherwise not clearly visible
1. 1 answer
2. 23 views