(Solved): USE C++ w/ stdio.h CIS217 Exercise \( 1.9 \quad \) Use Linear interpolation on flight path ta ...

USE C++ w/ stdio.h

CIS217 Exercise \( 1.9 \quad \) Use Linear interpolation on flight path table data Place comment headers on your code. Print the code and take a screen shot of your output Problem 43 (pg 78 in Etter), also see the flight path data table on the next sheet for input values This is an example display for this problem. Coefficient of Lift Interpolation Calculation Flight Path Begin Angle (Degrees) > Corresponding Coefficient of Lift > Flight Path End Angle (Degrees) > Corresponding Coefficient of Lift > Flight Path Desired Angle (between begin and end angle in Degrees) > Calculated Corresponding Coefficient of Lift: Notice this program accepts two inputs on one line with a space between them; this can also be programmed as two separate inputs on two lines depending on how you want to create the program. Make sure you use inputs that are part of the flight path data table as shown below examples This program uses linear interpolation to compute the coefficient of lift for an angle from a wind tunnel test Use degrees for all angle measurements. Enter first angle and lift coefficient with a space between them>14 \( 1.035 \) Enter second angle and lift coefficient with a space between them>15 \( 1.076 \) Enter new angle>14.3 New lift coefficient: \( 1.047 \) Figure \( 2.9 \) Wind tunnel data.