AEE 341 – Aerodynamics Project #1 “Calculation of Lift, Drag and Moment Coefficient” Faculty of Aeronautics and Astronautics The University of Turkish Aeronautical Association Dr. Kürşad Melih Güleren Instructions: 1. Lift, drag and moment coefficients of a NACA 0012 airfoil need to be calculated from a given pressure and skin coefficient distribution. 2. Required files can be downloaded from http://www.thk.edu.tr/~kmguleren/courses.html. 3. Please see the list of the angle of attack for student names. 4. A matlab or fortran code should be written to calculate lift, drag and moment coefficients. 5. Project reports and the code should be submitted via e-mail to Dr.Guleren no later than 7th of October 2014 11.59 pm. Late submission will not be accepted. 6. The project is not a bonus. It will affect 2.5 % of the overall grade. 7. Similar codes and reports as well as late submissions will be marked as ZERO. Student ID 120121058 120121025 120121024 120121007 120121048 120121602 120121604 120121617 120121618 120121619 120121620 120121622 120121626 130121401 120121050 120121614 Name Remzi Can Oðuzhan Kutay Ahmet Serkan Ali Volkan Naveed Habibul Bereket Sitotaw Mohamad Usama Mohamed Addow Rico Ahmed Idris Osman Mirza Meltem Andi Surname YILMAZ DEMİR ÇETİN ALTINOK ŞAHİN SULTAN ABRAR KIDANE KUNNATHUR MOHAMED MORASATA PRUŞEVİÇ SAMAILA YAHAYA DEMİRCAN ŞAHİN HOXHA -8 -7 -6 -5 -4 -3 -2 -1 1 2 3 4 5 6 7 8
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