From: To: <13015-M06@classes.uci.edu>; <13016-M06@classes.uci.edu>; <14315-M06@classes.uci.edu>; <14316-M06@classes.uci.edu>; <16325-M06@classes.uci.edu>; <16326-M06@classes.uci.edu> Subject: few points about final project for ENGR 80 Date: Thursday, August 24, 2006 1:30 AM A few points about the final project: Break down of grading for final project is as follows. 65% for analytical derivation: Where you need to clearly show the range as a function of initial angle, and LC. i.e. You need to write down what this function will look like. This should be the final result of your analytical derivation. It should all be in symbols. i.e. do not use ‘12’ in place of 'h' or '100' in place of 'Mc' and such. Just use symbols here. You need to show all the derivation used to obtain this function. 15% for presentation: The project should be typeset to get the full 15% for the presentation part. However, you can get a max of 10/15 if you just write it by hand as long as it is neatly done and I can read it. So if you find you will spend too much time on typing your report, I suggest you just write it by hand instead and spend the time studying for your final exams. 20% for code/method used to determine optimal design. For the final 20%. You do not need to generate a 3D plot to find the optimal solution. As we discussed in class, you can just check for the maximum in the code and keep track of it that way. The answer I get for the optimal design is as follows max range is 38.448410 meters, when initial_theta= 85.0 degrees and LC=2.500000 meters. Velocity=19.273435 m/s, time of flight=1.840586 seconds You can use any method you want to determine the final answer. You can use code it in Matlab or Mathematica or even Fortran. Nasser