Question: MATLAB program. This is a continuation of the discussion during module week 4: The same parachutist with a mass m of 80kg, a cross sectional
MATLAB program. This is a continuation of the discussion during module week 4: The same parachutist with a mass m of 80kg, a cross sectional area S of 0.65 m2, a drag coefficient CD = 0.45 at an atmospheric density at sea level = 1.225kg/m3 has an initial velocity of 0 m/s after dropping out of a balloon. Now, after falling for 15 seconds, he deploys the parachute. Which parameters change? Perform some research to find appropriate cross sectional areas and drag coefficients for civilian and military use. What is the main driver for sizing the parachute? Please help with the MATLAB code needed. I am awful at MATLAB and seriously need help with this. Please see attached image for details.
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