In a wind tunnel the pressure on the top surface of a model airplane wing is 8.8 *104 N/m and the pressure on the bottom surface is 9.0 * 104 N/m². If the area of the top and bottom surfaces of each wing is 2.0 m², what is the total lift on the model airplane? A)2.0 *103 N B)8.0 * 103 N C)1.6 * 104 N D)3.6 * 104 N E)1.0 * 103 N

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The Answer of In a wind tunnel the pressure on the top surface of a model airplane wing is 8.8 *104 N/m and the pressure on the bottom surface is 9.0 * 104 N/m². If the area of the top and bottom surfaces of each wing is 2.0 m², what is the total lift on the model airplane? A)2.0 *103 N B)8.0 * 103 N C)1.6 * 104 N D)3.6 * 104 N E)1.0 * 103 N

In a Wind Tunnel the Pressure on the Top Surface