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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 11 Review 17 CrossRef Cited 32 TR Dizin Cited 44
11 Publication
17 Review
32 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

9

2

1526

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7451

1

1

7451

Publications

0

227

0

309

0

321

0

610

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 718

0

718

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 7773

0

7773

2

1526

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 7451

1

7451

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 2448

0

2448

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 2157

0

2157

Publications

Maximization of Flight Performance of Eight-Rotor Multirotor with Differentiated Hub Angle
Published: 2024 , Journal of Aviation
DOI: 10.30518/jav.1490356
CITED 1 FAVORITE 0 TOTAL DOWNLOAD COUNT 227

1

0

227

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 610

6

0

610

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 718

4

0

718

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 4 FAVORITE 0 TOTAL DOWNLOAD COUNT 7773

4

0

7773

9

2

1526

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7451

1

1

7451

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 2157

7

0

2157

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