avatar
Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 8 Review 10 CrossRef Cited 20 TR Dizin Cited 37
8 Publication
10 Review
20 CrossRef Cited
37 TR Dizin Cited

Research Fields

Fluid Mechanics and Thermal Engineering Aerospace Engineering Air-Space Transportation

Institution

ERCİYES ÜNİVERSİTESİ

Popular Publications

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 6744

1

1

6744

4

1

916

Publications

0

104

0

400

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 445

0

445

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 5972

0

5972

1

916

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 6744

1

6744

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 2296

0

2296

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 1956

0

1956

Publications

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 4 FAVORITE 0 TOTAL DOWNLOAD COUNT 400

4

0

400

Stability Evaluation of a Fixed-Wing Unmanned Aerial Vehicle with Morphing Wingtip
Published: 2022 , Journal of Aviation
DOI: 10.30518/jav.1073417
CITED 2 FAVORITE 0 TOTAL DOWNLOAD COUNT 445

2

0

445

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 2 FAVORITE 0 TOTAL DOWNLOAD COUNT 5972

2

0

5972

4

1

916

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 6744

1

1

6744

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 1956

7

0

1956

Interactive Guide Tool
If you want to see the panel introduction, you can click Start Tour.