An airplane has a mass of 2.2×106 kg , and the air flows past the lower...
An airplane has a mass of 2.2×106 kg , and the air flows past the lower surface of the wings at 85 m/s . If the wings have a surface area of 1200 m2 , how fast must the air flow over the upper surface of the wing if the plane is to stay in the air?
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An airplane has a mass of 2.2×106 kg , and the air flows past
the lower...
An airplane has a mass of 2.1×106 kg , and the air flows past the lower...
An airplane has a mass of 2.1×106 kg , and the air flows past the lower surface of the wings at 96 m/s If the wings have a surface area of 1500 m2 , how fast must the air flow over the upper surface of the wing if the plane is to stay in the air? Express your answer to two significant figures and include the appropriate units.
An airplane has a mass of 10x10 kg, and the ar flows put the lower surface...
An airplane has a mass of 10x10 kg, and the ar flows put the lower surface of the wings at 82 m/s - Part A the wings have a surface area of 1300 ml how fast must the air flow over the upper surface of the wing if the plane Express your answer to two significant figures and include the appropriate units. JARO? Value
If air flows under the wing of.an 80,000 kg plane with a speed of 280 m/s...
If air flows under the wing of.an 80,000 kg plane with a speed of 280 m/s how fast does it need to flow over the top of the wing in order to keep the plane in the air if the wings have a surface area of 60 m2?
A small jet airplane has a total wing area of 62.5 m2 and a mass of...
A small jet airplane has a total wing area of 62.5 m2 and a mass of 7.03 104 kg. (a) If this jet is in horizontal flight, determine the pressure difference between the lower and upper surfaces of the wings. (b) When the speed of air traveling over the wing is 237 m/s, determine the speed of air under the wing. Use 1.29 kg/m3 as the density of air.
If the speed of flow past the lower surface of an airplane wing is 101 m/s,...
If the speed of flow past the lower surface of an airplane wing is 101 m/s, what speed of flow over the upper surface will give a pressure difference of 889 Pa between upper and lower surfaces? Take the density of air to be 1.30 × 10-3 g/cm3. Assume the lower surface is at the higher pressure.
PRACTICE IT Use the worked example above to help you solve this problem. An airplane has...
PRACTICE IT
Use the worked example above to help you solve this problem. An
airplane has wings, each with area 4.05 m2, designed so
that air flows over the top of the wing at 249 m/s and underneath
the wing at 226 m/s. Find the mass of the airplane such that the
lift on the plane will support its weight, assuming the force from
the pressure difference across the wings is directed straight
upwards.
Your response differs from the correct...
12. (10 points) Air streams horizontally past an airplane's wings such that the speed is 312.0...
12. (10 points) Air streams horizontally past an airplane's wings such that the speed is 312.0 m/s over the top surface and 300.0 m/s past the bottom surface. If the plane has a mass of 1.2x10 kg and a wing area of 300.0 m', what is the net vertical acceleration (including the effects of gravity) on the airplane? The density of the air is 1.20 kg/m'. g = 9.8 m/s?. (a) 0.72 m/s? (b) 0.92 m/s? (c) 1.22 m/s2 (d)...
Find the pressure difference on an airplane wing if air flows over the upper surface with...
Find the pressure difference on an airplane wing if air flows over the upper surface with a speed of 115 m/s , and along the bottom surface with a speed of 103 m/s . Answer is in kPa. If the area of the wing is 33 m2 , what is the net upward force exerted on the wing? Express your answer using two significant figures. Answer in kN
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 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.
Use the worked example above to help you solve this problem. An airplane has wings, each...
Use the worked example above to help you solve this problem. An airplane has wings, each with area 3.95 m2, designed so that air flows over the top of the wing at 249 m/s and underneath the wing at 225 m/s. Find the mass of the airplane such that the lift on the plane will support its weight, assuming the force from the pressure difference across the wings is directed straight upwards.
An airplane has a mass of 10x10 kg, and the ar flows put the lower surface of the wings at 82 m/s - Part A the wings have a surface area of 1300 ml how fast must the air flow over the upper surface of the wing if the plane Express your answer to two significant figures and include the appropriate units. JARO? Value
If air flows under the wing of.an 80,000 kg plane with a speed of 280 m/s how fast does it need to flow over the top of the wing in order to keep the plane in the air if the wings have a surface area of 60 m2?
PRACTICE IT
Use the worked example above to help you solve this problem. An
airplane has wings, each with area 4.05 m2, designed so
that air flows over the top of the wing at 249 m/s and underneath
the wing at 226 m/s. Find the mass of the airplane such that the
lift on the plane will support its weight, assuming the force from
the pressure difference across the wings is directed straight
upwards.
Your response differs from the correct...
12. (10 points) Air streams horizontally past an airplane's wings such that the speed is 312.0 m/s over the top surface and 300.0 m/s past the bottom surface. If the plane has a mass of 1.2x10 kg and a wing area of 300.0 m', what is the net vertical acceleration (including the effects of gravity) on the airplane? The density of the air is 1.20 kg/m'. g = 9.8 m/s?. (a) 0.72 m/s? (b) 0.92 m/s? (c) 1.22 m/s2 (d)...
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