Question: . An aircraft wing may be represented by a single horseshoe vortex of span 20 and circulation strength 25ms1. Calculate the downwash angle of
. An aircraft wing may be represented by a single horseshoe vortex of span 20 and circulation strength 25ms1. Calculate the downwash angle of a point 15 downstream of the bound vortex, in the plane of the vortex system on its centrelin The flight speed is 104 ms . (Answer: 0.4830).
Step by Step Solution
There are 3 Steps involved in it
To calculate the downwash angle we can use the formula ta... View full answer
Get step-by-step solutions from verified subject matter experts
