AEE 341 – Aerodynamics Project #2 “Calculation of Pressure Distribution on NACA 0012 using Source Panel Method” Faculty of Aeronautics and Astronautics The University of Turkish Aeronautical Association Dr. Kürşad Melih Güleren Instructions: 1. Pressure distribution on NACA 0012 airfoil needs to be calculated using a code 2. 3. 4. 5. 6. 7. 8. written based on Source Panel Method. Required files can be downloaded from http://www.thk.edu.tr/~kmguleren/courses.html. Please see the list of the angle of attack for student names. Each student is also responsible of calculation the pressure distribution at zero angle of attack. A matlab of fortran code should be written to calculate and plot the pressure distribution along with the pressure data given on the web site. Differences between the pressure distributions of source panel method and those of data given on the web site have to be discussed. Project reports and the code should be submitted via e-mail to Dr.Guleren no later than 9th of December 2014 11.59 pm. Late submissions will not be accepted. The project is not a bonus. It will affect 5 % of the overall grade. 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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# AEE 341 – Aerodynamics Project #2