when an aircraft or an automobile is moving through the atmosphere, it must over

Question

when an aircraft or an automobile is moving through the atmosphere, it must overcome a force called drag that works against the motion of the vehicle. the drag force can be expressed as
F=(1/2)CD*A*p*V2
where F is the force ( in newtons), CD is the drag coefficient, A is the project area of the vehicle perpendicular to the velocity vector ( in m2), p is the density of the gas or fluid through which the body is traveling (kg/m^3), and V is the body's velocity. the drag coefficient CD has a complex derivationand is frequently an empirical quantity. sometimes the drag coefficient has its own dependencies on velocities: For an automobile, the range is from approximately 0.2 ( for a very streamlined passenger vehicle) through about 0.5. for simplicity, assume a streamlined passenger vehicle is moving through air at sea level (where p= 1.23 kg/m^3). write a program that allows a user to input A and CD interactively and calls a function to compute the drag force. your program should display a table showing the drag force for the input shape for a range of velocities from 0 m/s to 40 m/s.

Explanation / Answer

DEAR FRIEND here is the program u want PLEASE RATE #include #include void calculate_drag_force(float A, float CD) { float F; float p=1.23; printf("%s %s ","Velocity Drag Force"); for(int i=0; i

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