Air is streaming past the wings of an acroplane with a speed of 90ms^(-1) below and 120ms^(-1) above the surface. If the wing is 15 m long and has an average width of 2m, then: Density of air =1.2kg//m^(3)]

Air is streaming past the wings of an acroplane with a speed of 90ms^(

1.	Air is streaming past the wings of an acroplane with a speed of 90ms^(-1) below and 120ms^(-1) above the surface. If the wing is 15 m long and has an average width of 2m, then: Density of air =1.2kg//m^(3)]
Answer» Pressure difference between the BOTTOM and top of he wing is4090 Pa Up - lift on the wing is 81900 N Up - lift on the wing is 113.58 K N Pressure difference between the bottom and top of wing is 3780 Pa Answer :C::D