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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 12 Review 18 CrossRef Cited 38 TR Dizin Cited 50
12 Publication
18 Review
38 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

11

2

1956

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8072

1

1

8072

Publications

0

359

0

397

0

640

0

460

0

800

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 954

0

954

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 8589

0

8589

2

1956

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 8072

1

8072

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 2593

0

2593

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 2293

0

2293

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 397

3

0

397

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 800

7

0

800

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 954

4

0

954

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 5 FAVORITE 0 TOTAL DOWNLOAD COUNT 8589

5

0

8589

11

2

1956

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 8072

1

1

8072

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 2293

7

0

2293