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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 11 Review 17 CrossRef Cited 34 TR Dizin Cited 44
11 Publication
17 Review
34 CrossRef Cited
44 TR Dizin Cited

Research Fields

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

Institution

ERCİYES ÜNİVERSİTESİ

Popular Publications

10

2

1614

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7526

1

1

7526

Publications

0

275

0

385

0

352

0

652

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 775

0

775

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 7909

0

7909

2

1614

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 7526

1

7526

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 2499

0

2499

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 2194

0

2194

Publications

Maximization of Flight Performance of Eight-Rotor Multirotor with Differentiated Hub Angle
Published: 2024 , Journal of Aviation
DOI: 10.30518/jav.1490356
CITED 2 FAVORITE 0 TOTAL DOWNLOAD COUNT 275

2

0

275

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 6 FAVORITE 0 TOTAL DOWNLOAD COUNT 652

6

0

652

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 775

4

0

775

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 4 FAVORITE 0 TOTAL DOWNLOAD COUNT 7909

4

0

7909

10

2

1614

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7526

1

1

7526

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 2194

7

0

2194

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