I'm in final year of my BE Aerospace. I'm currently desingning an aircraft as my final year project. I have done my prelimanary calculations. Now i want to simulate it and find Cl, Cd for my wing and fuslage design and eventually make them better.

Please help me, cause im new to all this and i need a good start.

Please mention some tutorial, books, examples or websites, or anything which can lead to my problem solution.

Go to the Cornell Fluent website. They have some good examples using Fluent.