Remove ads

Recently Taken
Ridhima kapoor
November 1, 2016
7,562 views 48 plays
1
A delta wing has
2
The Lift/Drag ratio of a wing at the stalling angle is
3
The airflow over the upper surface of a cambered wing
4
The speed of air over a swept wing which contributes to the lift is
5
In straight and level flight, the angle of attack of a swept wing is
6
Induced drag
7
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
8
The stagnation point is
9
If a swept wing stalls at the tips first, the aircraft will
10
The thickness/chord ratio of the wing is also known as
3
Like (3)
Loading...
3