Prof. Dr. MAHMUT ADİL YÜKSELEN

Yayın Ağı

Makaleler 13

1. A new nonlinear lifting line method for aerodynamic analysis and deep learning modeling of small unmanned aerial vehicles

Karali H., Inalhan G., Umut Demirezen M., Adil Yukselen M. A.

International Journal of Micro Air Vehicles , cilt.13, 2021 (SCI-Expanded, Scopus)

2. Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing

Aktas Y. O., Ozdemir U., Dereli Y., Tarhan A. F., Cetin A., Vuruskan A., et al.

Journal of Intelligent and Robotic Systems: Theory and Applications , cilt.84, sa.1-4, ss.639-664, 2016 (SCI-Expanded, Scopus)

3. UNSTEADY THERMAL STUDIES OF GUN BARRELS DURING THE INTERIOR BALLISTIC CYCLE WITH NON-HOMOGENOUS GUN BARREL MATERIAL THERMAL CHARACTERISTICS

AKÇAY M., YÜKSELEN M. A.

Isı Bilimi ve Tekniği Dergisi , cilt.34, sa.2, ss.75-81, 2014 (SCI-Expanded, TRDizin)

4. Computer assisted aerodynamics education

Yükselen M. A.

PROCEDIA SOCIAL AND BEHAVIOURAL SCIENCES , cilt.47, ss.362-368, 2012 (Düzenli olarak gerçekleştirilen hakemli kongrenin bildiri kitabı)

5. Flow of power-law fluids over a moving wedge surface with wall mass injection

Akçay M., Yükselen M. A.

Archive of Applied Mechanics , cilt.81, sa.1, ss.65-76, 2011 (SCI-Expanded, Scopus)

6. A unifying grid approach for solving potential flows applicable to structured and unstructured grid configurations

Çete A. R., Yükselen M. A., Kaynak Ü.

Computers and Fluids , cilt.37, sa.1, ss.35-50, 2008 (SCI-Expanded, Scopus)

7. Drag reduction of a nonnewtonian fluid by fluid injection on a moving wall

Akçay M., Adil Yükselen M. A.

Archive of Applied Mechanics , cilt.69, sa.3, ss.215-225, 1999 (SCI-Expanded, Scopus)

8. Basic equations for incompressible, non-Newtonian fluids in curvilinear, non-orthogonal and accelerated coordinate systems

Yükselen M. A.

ACTA MECHANICA , sa.118, ss.39-54, 1996 (Scopus)

9. Basic equations for incompressible, non-Newtonian fluids in curvilinear, non-orthogonal and accelerated coordinate systems

Yükselen M. A., Erim M.

Acta Mechanica , cilt.118, ss.39-54, 1996 (Scopus)

10. Superposition technique for two dimensional potential flow around multielement aerofoils

Yükselen M. A.

MECHANICS RESEARCH COMMUNICATIONS , cilt.23, sa.1, ss.103-110, 1996 (Scopus)

11. Superposition technique for potential flow around an aerofoil and control of the circulation

Yükselen M. A.

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS , cilt.0,22101310221996, ss.1013-1022, 1996 (Scopus)

12. The wind energy potential of Gökçeada in the Northern Aegean Sea

Yükselen M. A.

RENEWABLE ENERGY , cilt.6, sa.7, ss.679-685, 1995 (Scopus)

13. A general iterative method to design Kármán‐Trefftz and Joukowsky airfoils

Yükselen M. A., Erim M.

International Journal for Numerical Methods in Engineering , cilt.20, sa.7, ss.1349-1360, 1984 (Scopus)

Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 7

1. A novel physics informed deep learning method for simulation-based modelling

Karali H., Demirezen M. U., Yukselen M. A., Inalhan G.

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 Ocak 2021, ss.1-12, (Tam Metin Bildiri)

2. Design of a deep learning based nonlinear aerodynamic surrogate model for uavs

Karali H., Demirezen M. U., Yukselen M. A., Inalhan G.

AIAA Scitech Forum, 2020, Florida, Amerika Birleşik Devletleri, 6 - 10 Ocak 2020, cilt.1 PartF, ss.1-14, (Tam Metin Bildiri)

3. A GENETIC ALGORITHM BASED DESIGN OPTIMIZATION METHOD FOR WING-TAIL COMBINATIONS OF UAVs

Yıldız Ş., Yükselen M. A.

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019, ss.149, (Tam Metin Bildiri)

4. A PRACTICAL TOOL FOR DETERMINATION AND OBSERVATION OF 3D WING AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK

Karali H., Yükselen M. A.

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019, ss.147, (Tam Metin Bildiri)

5. A new non-linear lifting line method for 3D analysis of wing/configuration aerodynamic characteristics with application to UAVs

Karali H., Yukselen M. A., İnalhan G.

AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019, (Tam Metin Bildiri)

6. A low cost prototyping approach for design analysis and flight testing of the TURAC VTOL UAV

Aktas Y. O., Ozdemir U., Dereli Y., Tarhan A. F., Cetin A., Vuruskan A., et al.

2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014, Orlando, FL, Amerika Birleşik Devletleri, 27 - 30 Mayıs 2014, ss.1029-1039, (Tam Metin Bildiri)

7. Dynamic modeling of a fixed-wing VTOL UAV

Vuruskan A., Yuksek B., Ozdemir U., Yukselen A., İnalhan G.

2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014, Orlando, FL, Amerika Birleşik Devletleri, 27 - 30 Mayıs 2014, ss.483-491, (Tam Metin Bildiri)

Kitaplar 2

1.

Yükselen M. A., Vatandaş O. E.

AERODİNAMİĞİN ESASLARI (Fundamentals of Aerodynamics çevirisi), Yükselen, M. Adil, Editör, Nobel Akademik Yayıncılık, İstanbul, ss.1-560, 2024

2. UÇUŞA BAŞLANGIÇ

Yükselen M. A.

McGraw-Hill Companies , Ankara, 2020

Metrikler

Prof. Dr. MAHMUT ADİL YÜKSELEN

Yayınlar & Eserler

1. A new nonlinear lifting line method for aerodynamic analysis and deep learning modeling of small unmanned aerial vehicles

2. Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing

3. UNSTEADY THERMAL STUDIES OF GUN BARRELS DURING THE INTERIOR BALLISTIC CYCLE WITH NON-HOMOGENOUS GUN BARREL MATERIAL THERMAL CHARACTERISTICS

4. Computer assisted aerodynamics education

5. Flow of power-law fluids over a moving wedge surface with wall mass injection

6. A unifying grid approach for solving potential flows applicable to structured and unstructured grid configurations

7. Drag reduction of a nonnewtonian fluid by fluid injection on a moving wall

8. Basic equations for incompressible, non-Newtonian fluids in curvilinear, non-orthogonal and accelerated coordinate systems

9. Basic equations for incompressible, non-Newtonian fluids in curvilinear, non-orthogonal and accelerated coordinate systems

10. Superposition technique for two dimensional potential flow around multielement aerofoils

11. Superposition technique for potential flow around an aerofoil and control of the circulation

12. The wind energy potential of Gökçeada in the Northern Aegean Sea

13. A general iterative method to design Kármán‐Trefftz and Joukowsky airfoils

1. A novel physics informed deep learning method for simulation-based modelling

2. Design of a deep learning based nonlinear aerodynamic surrogate model for uavs

3. A GENETIC ALGORITHM BASED DESIGN OPTIMIZATION METHOD FOR WING-TAIL COMBINATIONS OF UAVs

4. A PRACTICAL TOOL FOR DETERMINATION AND OBSERVATION OF 3D WING AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK

5. A new non-linear lifting line method for 3D analysis of wing/configuration aerodynamic characteristics with application to UAVs

6. A low cost prototyping approach for design analysis and flight testing of the TURAC VTOL UAV

7. Dynamic modeling of a fixed-wing VTOL UAV

1.

2. UÇUŞA BAŞLANGIÇ

Yayın

Yayın (WoS)

Yayın (Scopus)

Atıf (Scopus)

H-İndeks (Scopus)

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