What force would be required to accelerate a 1100 kg car to 0 5 m/s2

Determine the maximum r-value of the polar equation r =3+3 cos 0

The ratio of lift to drag l/d for a wing or airfoil is an important aerodynamic parameter, indeed, it is a direct measure of the aerodynamic efficiency of the wing. if a wing is pitched through a range of angle of attack, l/d first increases, then goes through a maximum, and then decreases. consider an infinite wing with an naca 2412 airfoil. estimate the maximum value of l/d. assume that the reynolds number is 9x10^6.

When the magnetic domains in a material can be aligned, but eventually drift out of alignment, the material is