An aircraft is designed with lift coefficient of 1.1 during steady level flight. If dynamic pressure is set to be 25.65 Pa then find weight of aircraft during this flight condition.

An aircraft is designed with lift coefficient of 1.1 during steady lev

1.	An aircraft is designed with lift coefficient of 1.1 during steady level flight. If dynamic pressure is set to be 25.65 Pa then find weight of aircraft during this flight condition.
A.	28.215 N per unit area
B.	30 kg
C.	59 N
D.	125.25 N
Answer» B. 30 kg

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An aircraft is designed with lift coefficient of 1.1 during steady level flight. If dynamic pressure is set to be 25.65 Pa then find weight of aircraft during this flight condition.

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