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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 14 Review 19 CrossRef Cited 41 TR Dizin Cited 50
14 Publication
19 Review
41 CrossRef Cited
50 TR Dizin Cited

Research Fields

Fluid Mechanics and Thermal Engineering Air-Space Transportation Aerospace Engineering Aircraft Performance and Flight Control Systems

Institution

ERCİYES ÜNİVERSİTESİ

Popular Publications

12

2

2329

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8342

1

1

8342

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 5 FAVORITE 1 TOTAL DOWNLOAD COUNT 9013

5

1

9013

Publications

Stability Based Modeling of Double Dihedral and Double Sweep Wing UAV
Published: 2026 , Journal of Aviation
DOI: 10.30518/jav.1895788
FAVORITE 0 TOTAL DOWNLOAD COUNT 97

0

97

0

601

0

526

0

846

0

743

0

968

Stability Evaluation of a Fixed-Wing Unmanned Aerial Vehicle with Morphing Wingtip
Published: 2022 , Journal of Aviation
DOI: 10.30518/jav.1073417
FAVORITE 0 TOTAL DOWNLOAD COUNT 1152

0

1152

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 1 TOTAL DOWNLOAD COUNT 9013

1

9013

2

2329

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 8342

1

8342

Autonomous flight performance improvement of the morphing aerial robot by aerodynamic shape redesign
Authors: Harun Çelik , Tuğrul Oktay , Metin Uzun
DOI: 10.16984/saufenbilder.362588
FAVORITE 0 TOTAL DOWNLOAD COUNT 2706

0

2706

A novel learning algorithm to estimate the optimum fuselage drag coefficient
Authors: Tuğrul Oktay , Harun Çelik , Metin Uzun
DOI: 10.16984/saufenbilder.290738
FAVORITE 0 TOTAL DOWNLOAD COUNT 2359

0

2359

Publications

1

0

601

Maximization of Flight Performance of Eight-Rotor Multirotor with Differentiated Hub Angle
Published: 2024 , Journal of Aviation
DOI: 10.30518/jav.1490356
CITED 3 FAVORITE 0 TOTAL DOWNLOAD COUNT 526

3

0

526

Effects of Shape Changing of Morphing Rotary Wing Aircraft on Longitudinal and Lateral Flight
Published: 2022 , Journal of Aviation
DOI: 10.30518/jav.1080139
CITED 8 FAVORITE 0 TOTAL DOWNLOAD COUNT 968

8

0

968

Stability Evaluation of a Fixed-Wing Unmanned Aerial Vehicle with Morphing Wingtip
Published: 2022 , Journal of Aviation
DOI: 10.30518/jav.1073417
CITED 4 FAVORITE 0 TOTAL DOWNLOAD COUNT 1152

4

0

1152

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 5 FAVORITE 1 TOTAL DOWNLOAD COUNT 9013

5

1

9013

12

2

2329

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8342

1

1

8342

A novel learning algorithm to estimate the optimum fuselage drag coefficient
Authors: Tuğrul Oktay , Harun Çelik , Metin Uzun
DOI: 10.16984/saufenbilder.290738
CITED 7 FAVORITE 0 TOTAL DOWNLOAD COUNT 2359

7

0

2359