Using Recursive Method:
- Write A C Program Using Recursive Method Plz Help Me Tysm 1 (54.75 KiB) Viewed 89 times
Write a program to determine the lift force created on a wing of an airplane using the following detail: 1. The wing is a square plate 10 m X 5 m 2. The pressure values at the top of the plate are read from the supplied data in the form of a table. The plate is subdivided into smaller rectangles 2 mx1 m. The air pressure acts downward on the wing. Assume that the air pressure on each smaller rectangle is uniform. So the force pushing down on the small rectangles is just pressure * Area. 3. Similarly, the air pressure acting at the bottom of the wing (plate) is read from the supplied data. The bottom of the plate is also subdivided into smaller rectangles as the top. 4. Calculate the total force acting downward and the total force acting upward on the wing. 5. Subtract these two forces to obtain the lift force in newton. You must use the recursive technique in calculating the lift. Note that you will be needing to calculate force for each small rectangle and add them up. This lends itself to a recursive operation. Table 1Pressure distribution over the bottom of the wing (kPa). Each box represents pressure over the smaller rectangle. 2 meter 100 100 100 100 100 1 meter 2 meter 3 meter 4 meter 4 meter 100 96 100 99 95 6 meter 95 97 95 88 90 8 meter 95 88 95 77 85 10 meter 80 85 85 70 80 J 5 meter
Table 2Pressure distribution over the top of the wing (KPa). Each box represents pressure over the smaller rectangle. 1 meter 2 meter 3 meter 4 meter 5 meter 2 meter 5 5 5 5 5 ՄՄ |Մ|Մ՝ 4 meter 8 5 7 5.5 6 6 meter 5 6 5 6.5 6.5 8 meter 5.5 5 6 5 5.5 ת סתU 10 meter 5 6.0 5.5 5 5