For the wing foil, dtermine the aerodynamic lift. density
ofair=1.21 kg/m3. area= 200m2.
speed=150m/s, speed=100m/s.

The lift is the force generated on a body that travels through a fluid, perpendicular to the speed of the incident current. The mathematical model is given as

Here,

= Density

A = Cross sectional Area

=  Upper Velocity

= Down Velocity

Our values are given as

=1.21 kg/m3.

A= 200m2.

=150m/s

=100m/s

Replacing we have,

Therefore the areodynamic lift would be

get the total number of pieces of fruit and divide it by 4 to get the average. the result is the answer to the problem. 14 total number of fruits and there are 4 members. 14 divided by 4 is equals to 3.5.

in order to follow the instructions and complete the statements, i need to use data from table c of your student guide. can you think of a way to let me see your student guide for a while ? i can't answer the question without the data in table c.