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Tuğrul Oktay Prof. Dr. ERCİYES ÜNİVERSİTESİ
Publication 8 Review 11 CrossRef Cited 20 TR Dizin Cited 37
8 Publication
11 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 6756

1

1

6756

4

1

945

Publications

0

107

0

403

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 449

0

449

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
FAVORITE 0 TOTAL DOWNLOAD COUNT 6041

0

6041

1

945

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
FAVORITE 1 TOTAL DOWNLOAD COUNT 6756

1

6756

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 2299

0

2299

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 1962

0

1962

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 403

4

0

403

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 449

2

0

449

System Design and Control of Rotary Wing Unmanned Aerial Vehicle
DOI: 10.31590/ejosat.957056
CITED 2 FAVORITE 0 TOTAL DOWNLOAD COUNT 6041

2

0

6041

4

1

945

Morphinglet Wing Tip Design and Advantages
DOI: 10.31590/ejosat.634822
CITED 1 FAVORITE 1 TOTAL DOWNLOAD COUNT 6756

1

1

6756

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 1962

7

0

1962

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