If an aircraft is operating with dynamic pressure of the free stream q=20Pa and has area of wing is 10m2 then evaluate drag experience by the aircraft. Given drag coefficient is 0.9.
If an aircraft is operating with dynamic pressure of the free stream q=20Pa and has area of wing is 10m2 then evaluate drag experience by the aircraft. Given drag coefficient is 0.9. Correct Answer 180 N
Given, free stream q=20Pa, area of wing S = 10m2, drag coefficient CD = 0.9 Drag D = q*S*CD = 20*10*0.9 = 180N.
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Feb 20, 2025