PROJECT 3: Matlab Programming

Problem Statement

Determine the ground roll takeoff distance using
a) ode23
b) ode45

Use T=1000[55.6-4.6(V/100)+.357(V/100)^2] for each engine.

Submit standard report including

  1. source codes
  2. input files
  3. plot of speed vs distance  from Project 2c part  d)

    4. on same plot with present results.

     

Due:  Feb 23, 10AM