Basic equation applicable = P + 0.5
v^2
a) if both the wings are at same height, the velocity will same resulting in null pressure difference
b) Pbottom - Ptop = 0.5
( 245^2 - 222^2) =
0.5 ( 1.29 ) ( 60025 - 49284) =6927. 945 Pascals
c) Lift forc e= 6927. 945( 4) =27711.78 N
d) lift is directly proportional to dnsity, mars density is less than earth's so an airplane will experience less lift
e
An airplane wing generates lift due to a difference in air speed above and below the...
5. (a) (5 pts) The lift of an airplane wing is the difference in pressure above and below the wings times the area of the wing. How much lift is generated by a wing with an area of 16.2 square meters and an average pressure differential of 675 Nim (675 pascals) between the top and bottom of the wing? (b) (5 pts) How much cargo could a plane with this much lift carry if the empty plane has a mass...
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.
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.
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...
An airplane has an effective wing surface area of 21.9 m2 that is generating the lift force. In level flight the air speed over the top of the wings is 70.0 m/s, while the air speed beneath the wings is 47.0 m/s. What is the weight of the plane?
An airplane wing was designed so that the speed of the air across the wing is 248 m/s when the speed of the air below the wing is 194 m/s. The density of the air is 1.29 kg/m^3. What is the lifting force on a wing of area 23.0 m^2?
The substantial lift force on the wing of a flying airplane is due to the fact that the wing -is typically made of a special gravity-defiant material. -is in fact moving more slowly than the air surrounding it. -is moving rapidly enough to produce a pressure difference between above and below the wing. -increases the kinetic energy of air particles all around the wing. -has weight that is less than the buoyant force from air.
An airplane wing is designed so that the speed of the air across the top of the wing is 283 m/s when the speed of the air below the wing is 223 m/s. The density of the air is 1.29 kg/m3. What is the lifting force on a wing of area 22.0 m2?
An air-plane has an effective wing surface area of 12.0 m² that is generating the lift force. In level flight the air speed over the top of the wings is 65.5 m/s, while the air speed beneath the wings is 39.0 m/s. What is the weight of the plane?(The density of air is 1.29 kg/m³)