avatar
Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 11 Review 12 CrossRef Cited 26 TR Dizin Cited 44
11 Publication
12 Review
26 CrossRef Cited
44 TR Dizin Cited

Research Fields

Fluid Mechanics and Thermal Engineering Aerospace Engineering Air-Space Transportation

Institution

ERCİYES ÜNİVERSİTESİ

Popular Publications

6

2

1203

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7022

1

1

7022

Publications

0

41

0

104

0

181

0

503

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 559

0

559

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 6633

0

6633

2

1203

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 7022

1

7022

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 2374

0

2374

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 2051

0

2051

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 503

4

0

503

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 559

4

0

559

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 4 FAVORITE 0 TOTAL DOWNLOAD COUNT 6633

4

0

6633

6

2

1203

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 7022

1

1

7022

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 2051

7

0

2051

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