Calculate the standard sealevel turn rate that the A10 airpl

Calculate the standard sea-level turn rate that the A-10 airplane can achieve when flying at its corner speed of 110 m/s.

The A-10 has wing area = 47 m2, maximum lift coefficient = 1.2, and weight = 103,000 N.

a. 0.35 deg/s c. 19.8 deg/s b. 16.5 deg/s d. 34.1 deg/s

please help me solve this question with detail answers!

Solution

From the above given data sea level turn rate can be calculated in the following manner

47*103000/1.2

=19.8 degree/s