Introduction to Computational Physics Using C/C++/Matlab

Computational Physics (2nd Edition) 2nd Edition By Nicholas J. Giordano

Problem 2.1 Use the Euler method to calculate cannon shell trajectories ignoring both air drag and the effect of air density (actually ignoring the former automatically rules out the latter). Compare your results with the exact solution. Please write the program in C or C++ or Matlab and include many comments and explanatory notes which explain the reasoning behind the construction and structure of your source code.