Question: Assuming elliptical lift distribution and a rectangular wing with span of 11.5m, find the ratio of C (Overall wing) to cl (aerofoil section) at

Assuming elliptical lift distribution and a rectangular wing with span of 11.5m, find the ratio of C (Overall

Assuming elliptical lift distribution and a rectangular wing with span of 11.5m, find the ratio of C (Overall wing) to cl (aerofoil section) at a spanwise L position 0.32 measured as a fraction of the overall semi-span from the centre. Take I to be 59, give your answer to 2dp: 0

Step by Step Solution

3.49 Rating (156 Votes )

There are 3 Steps involved in it

1 Expert Approved Answer
Step: 1 Unlock

Solution To find the ratio of C to cl we need to use the lift distribution equation for an elliptical lift distribution L 12 C R2 S 1 RS212 where L li... View full answer

blur-text-image
Question Has Been Solved by an Expert!

Get step-by-step solutions from verified subject matter experts

Step: 2 Unlock
Step: 3 Unlock

Students Have Also Explored These Related Accounting Questions!