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Seyhun Durmuş Assoc. Prof. Dr. BALIKESİR ÜNİVERSİTESİ
Publication 14 Review 12 CrossRef Cited 7
14 Publication
12 Review
7 CrossRef Cited

Research Fields

Aerodynamics (Excl. Hypersonic Aerodynamics) Computational Methods in Fluid Flow, Heat and Mass Transfer (Incl. Computational Fluid Dynamics) Aerospace Engineering Air-Space Transportation Aircraft Performance and Flight Control Systems

Institution

BALIKESİR ÜNİVERSİTESİ

Popular Publications

Numerical Analysis of NACA 6409 and Eppler 423 Airfoils
Published: 2023 , Journal of Polytechnic
DOI: 10.2339/politeknik.959517
CITED 0 FAVORITE 2 TOTAL DOWNLOAD COUNT 5154

0

2

5154

Aerodynamic Performance Comparison of Airfoils in Flying Wing UAV
DOI: 10.46460/ijiea.1169652
CITED 3 FAVORITE 2 TOTAL DOWNLOAD COUNT 6978

3

2

6978

Investigation of Wing, Fuselage and Tail Design Parameters in Boeing and Airbus Aircraft
DOI: 10.31590/ejosat.1017730
CITED 0 FAVORITE 1 TOTAL DOWNLOAD COUNT 5084

0

1

5084

0

1

873

Optimization of contraction cone length in an open-circuit wind tunnel
DOI: 10.25092/baunfbed.1339334
CITED 0 FAVORITE 1 TOTAL DOWNLOAD COUNT 227

0

1

227

Publications

Statistical Analysis of Airfoil Usage in Aircraft
Published: 2024 , Journal of Aviation
DOI: 10.30518/jav.1493359
FAVORITE 0 TOTAL DOWNLOAD COUNT 266

0

266

1

227

2

6978

Numerical Analysis of NACA 6409 and Eppler 423 Airfoils
Published: 2023 , Journal of Polytechnic
DOI: 10.2339/politeknik.959517
FAVORITE 2 TOTAL DOWNLOAD COUNT 5154

2

5154

Relationship Between Wingspan and Fuselage Length in Aircraft According to Engine Types
Published: 2023 , Journal of Aviation
DOI: 10.30518/jav.1163494
FAVORITE 0 TOTAL DOWNLOAD COUNT 2558

0

2558

1

873

Investigation of Wing Forms Through Mass and Wing Area Chart
DOI: 10.46810/tdfd.1084396
FAVORITE 0 TOTAL DOWNLOAD COUNT 1450

0

1450

Investigation of Wing, Fuselage and Tail Design Parameters in Boeing and Airbus Aircraft
DOI: 10.31590/ejosat.1017730
FAVORITE 1 TOTAL DOWNLOAD COUNT 5084

1

5084

Numerical Investigation of Effusion Cooling in Gas Turbine Combustor Liner
Published: 2021 , Journal of Aviation
DOI: 10.30518/jav.973603
FAVORITE 0 TOTAL DOWNLOAD COUNT 729

0

729

Effect of Rib Shape on Flow Regime and Heat Transfer
DOI: 10.34248/bsengineering.882373
FAVORITE 0 TOTAL DOWNLOAD COUNT 380

0

380

0

1935

Unpowered Flight Principle: Sailplane
Published: 2019 , Mühendis ve Makina
DOI: -
FAVORITE 0 TOTAL DOWNLOAD COUNT 2266

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2266

Publications

Aerodynamic Performance Comparison of Airfoils in Flying Wing UAV
DOI: 10.46460/ijiea.1169652
CITED 3 FAVORITE 2 TOTAL DOWNLOAD COUNT 6978

3

2

6978

Numerical Investigation of Effusion Cooling in Gas Turbine Combustor Liner
Published: 2021 , Journal of Aviation
DOI: 10.30518/jav.973603
CITED 1 FAVORITE 0 TOTAL DOWNLOAD COUNT 729

1

0

729

3

0

1935

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