Transition flight modeling of a fixed-wing VTOL UAV B Yuksek, A Vuruskan, U Ozdemir, MA Yukselen, G Inalhan Journal of Intelligent & Robotic Systems 84, 83-105, 2016 | 148 | 2016 |
Dynamic modeling of a fixed-wing VTOL UAV A Vuruskan, B Yuksek, U Ozdemir, A Yukselen, G Inalhan 2014 international conference on unmanned aircraft systems (ICUAS), 483-491, 2014 | 72 | 2014 |
Drag reduction of a nonnewtonian fluid by fluid injection on a moving wall M Akcay, MA Yükselen Archive of Applied Mechanics 69, 215-225, 1999 | 70 | 1999 |
The wind energy potential of Gökçeada in the northern Aegean Sea S Tolun, S Menteş, Z Aslan, MA Yükselen Renewable Energy 6 (7), 679-685, 1995 | 66 | 1995 |
Rapid prototyping of a fixed-wing VTOL UAV for design testing YO Aktas, U Ozdemir, Y Dereli, AF Tarhan, A Cetin, A Vuruskan, B Yuksek, ... Journal of Intelligent & Robotic Systems 84, 639-664, 2016 | 48 | 2016 |
A low cost prototyping approach for design analysis and flight testing of the turac vtol uav YO Aktas, U Ozdemir, Y Dereli, AF Tarhan, A Cetin, A Vuruskan, B Yuksek, ... 2014 International Conference on Unmanned Aircraft Systems (ICUAS), 1029-1039, 2014 | 37 | 2014 |
Unsteady thermal studies of gun barrels during the interior ballistic cycle with non-homogenous gun barrel material thermal characteristics M Akcay, MA Yükselen J. Therm. Sci. Technol 34 (2), 75-81, 2014 | 27 | 2014 |
Design of a deep learning based nonlinear aerodynamic surrogate model for UAVs H Karali, MU Demirezen, MA Yukselen, G Inalhan AIAA Scitech 2020 forum, 1288, 2020 | 21 | 2020 |
Aerodinamik ders notları MA Yükselen İTÜ, 2006 | 16 | 2006 |
A unifying grid approach for solving potential flows applicable to structured and unstructured grid configurations AR Çete, MA Yükselen, Ü Kaynak Computers & fluids 37 (1), 35-50, 2008 | 10 | 2008 |
Flow of power-law fluids over a moving wedge surface with wall mass injection M Akçay, MA Yükselen Archive of Applied Mechanics 81, 65-76, 2011 | 9 | 2011 |
Experimental investigation of a diffuser for cooling and air conditioning system V Bayramgil, S Bayrak, MA Yükselen, MZ Erim 21st Congress of the International Council of the Aeronautical Sciences …, 1998 | 9 | 1998 |
A general iterative method to design Kármán‐Trefftz and Joukowsky airfoils MA Yükselen, MZ Erim International journal for numerical methods in engineering 20 (7), 1349-1360, 1984 | 9 | 1984 |
A novel physics informed deep learning method for simulation-based modelling H Karali, UM Demirezen, MA Yukselen, G Inalhan AIAA Scitech 2021 Forum, 0177, 2021 | 8 | 2021 |
A new non-linear lifting line method for 3D analysis of wing/configuration aerodynamic characteristics with application to UAVs H Karali, MA Yükselen, G Inalhan AIAA Scitech 2019 forum, 2119, 2019 | 8 | 2019 |
Basic equations for incompressible, non-Newtonian fluids in curvilinear, non-orthogonal and accelerated coordinate systems MA Yükselen, MZ Erim Acta mechanica 118 (1), 39-54, 1996 | 8 | 1996 |
Computer assisted aerodynamics education MA Yukselen Procedia-Social and Behavioral Sciences 47, 362-368, 2012 | 6 | 2012 |
HM504 uygulamalı sayısal yöntemler ders notları MA Yükselen | 4 | 2008 |
Prediction of Wind Tunnel Wall Effects Using Panel Methods Y Demiroglu, MA Yukselen 10th Ankara international aerospace conference, AIAC, 2019 | 3 | 2019 |
A Genetic Algorithm Based Design Optimization Method for Wing-Tail Combinations of UAVs S Yildiz, MA Yukselen Ankara International Aerospace Conference, Ankara, 2019 | 2 | 2019 |