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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 12 Review 18 CrossRef Cited 39 TR Dizin Cited 50
12 Publication
18 Review
39 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

2048

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8153

1

1

8153

Publications

0

429

0

424

0

739

0

492

0

827

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 1008

0

1008

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 8733

0

8733

2

2048

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 8153

1

8153

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 2616

0

2616

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 2309

0

2309

Publications

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 424

3

0

424

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 7 FAVORITE 0 TOTAL DOWNLOAD COUNT 827

7

0

827

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 1008

4

0

1008

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 5 FAVORITE 0 TOTAL DOWNLOAD COUNT 8733

5

0

8733

12

2

2048

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8153

1

1

8153

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 2309

7

0

2309