The flow speed of air above the aircraft wing is v1 and below the aircraft wing is v2, then which of the following is correct for the dynamic lift of the aircraft?

1
v1 > v2
2
v1 < v2
3
v1 = v2
4
Can't say

Sponsored

hivanix.in

Visit

This quiz is brought to you by hivanix.in

🌐 Web App Development

Quick Navigation