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AEE 341 – Aerodynamics Project #1

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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

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Author
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