Ask Question
2 February, 16:01

How do you calculate the dynamic lift in an aeroplane?

+1
Answers (1)
  1. 2 February, 16:15
    0
    the lift equation states that lift L is equal to the lift coefficient CI times the density r times half of the velocity V squared times the wing area A. For given air conditions, shape and inclination of the object, we have to determine a value of CI to determine the lift.

    Not really sure but this is all I know
Know the Answer?
Not Sure About the Answer?
Find an answer to your question 👍 “How do you calculate the dynamic lift in an aeroplane? ...” in 📗 Engineering if the answers seem to be not correct or there’s no answer. Try a smart search to find answers to similar questions.
Search for Other Answers