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Departments  › Astronautical Engineering  › Academic Staff  › Dr. İdil FENERCİOĞLU

Phone: +90 212 285 31 46
Fax: +90 212 285 3140
Web Page:  
ITU Faculty of Aeronautics and Astronautics,
Department of Astronautical Engineering
Maslak 34469  İstanbul, Turkey


BSc Astraonautical Engineering, ITU, Turkey, 1999
MSc: Astraonautical Engineering, ITU, Turkey, 2002
PhD: Aerospace Engineering, ITU, Turkey, (2010)

Brief Resume

Born in Istanbul on 1977 and after finishing Beyoglu Anadolu Lisesi enrolled in ITU Space Engineering Programme in 1995. Acquired M.Sc. degree and started Aerospace Engineering PhD programme in 2002. Stayed in RWTH-Aachen Stosswellenlabor (Germany) as a visiting research fellow between October 2006-July 2007 and is currently a PhD student and research assistant at the Trisonic Research Laboratory. Interested in experimental aerodynamics and measurement techniques.

Principle Publications

  • Ozbilen A. C., Fenercioglu I., Zaloglu B., and Cetiner O., 2009: The Effect of a Flexible Extension on a Pitching SD7003 Foil in Steady Current. 5th Ankara International Aerospace Conference, August 17-19, 2009 METU, Ankara, Turkey.
  • Fenercioglu I., and Cetiner O., 2008: Flow Structures around an Oscillating Airfoil in Steady Current. 14th International Symposium on Applications of Laser Techniques to Fluid Mechanics, July 06-11, 2008 Lisbon, Portugal.
  • Luo X., Olivier H., and Fenercioglu I., 2008: The Generation of High Particle Velocities by Shock Tunnel Technology for Coating Application. 26th International Symposium on Shock Waves, July 15-20, 2007 German Aerospace Center (DLR), Göttingen, Germany. DOI: 10.1007/978-3-540-85181-3_15.
  • Fenercioglu I., and Yuceil K. B., 2006: Determination of Shock Oscillation Character by Instantaneous Imaging of Bow Shock Wave Caused by a Projectile. 12th International Symposium on Flow Visualization, September 10-14, 2006 German Aerospace Center (DLR), Göttingen, Germany.
  • Gunes H.,  Fenercioglu I., and Yuceil K. B., 2004: Instantaneous Imaging of Highly Unstable Bow Shock Wave Caused by a Hypervelocity Projectile With a Streamwise Nose Cavity. 11th International Symposium on Flow Visualization, August 9 - 12, 2004 University of Notre Dame, Notre Dame, Indiana, USA.