Publications & Works

Articles Published in Journals That Entered SCI, SSCI and AHCI Indexes

Articles Published in Other Journals

Yüksek Performanslı Kumaş Zırhların Balistik Dayanımlarının Sayısal Olarak İncelenmesi

Tekstil ve Mühendis, vol.24, no.105, pp.2-12, 2017 (National Refreed University Journal)

Computational ballistic impact analysis of aircraft armors

Journal of Aeronautics and Space Technologies, vol.10, no.1, pp.81-95, 2017 (International Refereed University Journal)

The effect of sweep angle on the limit cycle oscillations of aircraft wings

ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, vol.2, no.2, pp.199-215, 2015 (Journal Indexed in ESCI) identifier identifier

Refereed Congress / Symposium Publications in Proceedings

Computational Analysis of Orbital Debris Impact on Spacecraft Shields

8th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 19 - 22 June 2017, pp.235-240 identifier

Active vibration control applications for adaptive aircraft wings modelled as thin-walled composite beams

57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, California, United States Of America, 4 - 08 January 2016 identifier

Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin Walled Composite Beams

The 6th International Conference on Mechanical and Aerospace Engineering-ICMAE, 16 - 17 July 2015

Aeroleastic analysis of a thin-walled composite aircraft wing with an external store subjected to a follower force

ASME-IMECE2014-38479, International Mechanical Engineering Congress Exposition, 14 - 20 November 2014

ACTIVE VIBRATION CONTROL OF AIRCRAFT WINGS MODELED AS THIN-WALLED COMPOSITE BEAMS USING PIEZOELECTRIC ACTUATION

ASME International Mechanical Engineering Congress and Exposition (IMECE), Montreal, Canada, 14 - 20 November 2014 identifier identifier

DYNAMIC AND AEROELASTIC ANALYSES OF A WIND TURBINE BLADE MODELED AS A THIN-WALLED COMPOSITE BEAM

ASME International Mechanical Engineering Congress and Exposition (IMECE), Montreal, Canada, 14 - 20 November 2014 identifier

AEROELASTIC ANALYSIS OF A THIN-WALLED COMPOSITE AIRCRAFT WING WITH AN EXTERNAL STORE SUBJECTED TO A FOLLOWER FORCE

ASME International Mechanical Engineering Congress and Exposition (IMECE), Montreal, Canada, 14 - 20 November 2014 identifier

GEOMETRICALLY NONLINEAR VIBRATION ANALYSIS OF THIN-WALLED. COMPOSITE BEAMS

ASME International Mechanical Engineering Congress and Exposition (IMECE2013), California, United States Of America, 15 - 21 November 2013 identifier

Aeroelastic instability of aircraft wings modeled as thin-walled composite beams

7th Ankara International Aerospace Conference, 11 - 13 September 2013

OK AÇILI UÇAK KANATLARININ DOĞRUSAL OLMAYAN AEROELASTİK ANALİZİ

IV. Ulusal Havacılık Ve Uzay Konferansı, Turkey, 12 - 14 September 2012

Flutter Analysis of Goland Wing via Finite Element Method

6th Ankara International Aerospace Conference, Ankara, Turkey, 14 - 16 September 2011

Vibration analysis of rotating thin-walled composite beam via finite element method

International Forum of Aeroelasticity and Structural Dynamics, IFASD 2011, 26 - 30 June 2011

Approximate Analytical Soluti ons of Nonlinear Flutt er of Aircraft Wings

International Forum of Aeroelasticity and Structural Dynamics, IFASD 2011, 26 - 30 June 2011

Free Vibration Analysis of Rotating Thin-Walled Composite Beams

5th International Conference on Recent Advances in Space Technologies, Rast 2011, 9 - 11 June 2011

Finite Element Analysis of A Thin Walled Composite Wing by Including Warping Effects

2010 ASME International Mechanical Engineering Congress and Exposition, Vancouver, Canada, 12 - 18 November 2010

İnce Cidarli Kompozit Bir Kirişin Statik ve Dinamik Davranışı

III. Ulusal Havacılık Ve Uzay Konferansı, Turkey, 16 - 18 September 2010

FREE VIBRATION OF AN ANISOTROPIC THIN-WALLED BOX BEAM UNDER BENDING-TORSION COUPLING

3rd International Conference on Integrity, Reliability and Failure, 20 - 24 July 2009

Sesaltı Bir Kanadın Pk Metodu ile Flutter Analizi

Kayseri VII. Havacılık Sempozyumu, Kayseri, Turkey, 15 - 16 May 2008

Aeroelastic Analysis of a Tapered Aircraft Wing

4. Ankara International Aerospace Conference, 10-12 September 2007, 10 - 12 September 2007