For an airplane in flight, the average speed of the air relative
to the plane is 317 m/s below the wings and 348 m/s above the
wings. The bottom of each wing has a surface area of 29.9
m2. Calculate the lift, which is the net upward force of
air on the plane.
vb =317 m/s , va =348 m/s
Ab = 29.9 m^2
density of air d = 1.2 kg/m^3
Volume flow rate is constant
vb*Ab = va*Aa
Aa = vb*Ab/va = (317*29.9)/348
Aa = 27.24 m^2
F =PA
P = (1/2)dv^2
Net force Fb -Fa = (1/2)dvb2Ab - (1/2)dva2Aa
= (1/2)(1.2) [ (348*348*27.24) - (317*317*29.9)]
Fnet =1.77x105 N
For an airplane in flight, the average speed of the air relative to the plane is...
For an airplane in flight, the average speed of the air relative to the plane is 306 m/s below the wings and 336 m/s above the wings (see the figure below). The bottom of each wing has a surface area of 29.7 m2. Calculate the lift, which is the net upward force of air on the plane.
For an airplane in flight, the average speed of the air relative to the plane is 320 m/s below the wings and 352 m/s above the wings (see the figure below). The bottom of each wing has a surface area of 30.9 m2. Calculate the lift, which is the net upward force of air on the plane.
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