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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 5400

0

2

5400

Aerodynamic Performance Comparison of Airfoils in Flying Wing UAV
DOI: 10.46460/ijiea.1169652
CITED 3 FAVORITE 2 TOTAL DOWNLOAD COUNT 7421

3

2

7421

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 5327

0

1

5327

0

1

925

Optimization of contraction cone length in an open-circuit wind tunnel
DOI: 10.25092/baunfbed.1339334
CITED 0 FAVORITE 1 TOTAL DOWNLOAD COUNT 298

0

1

298

Publications

Statistical Analysis of Airfoil Usage in Aircraft
Published: 2024 , Journal of Aviation
DOI: 10.30518/jav.1493359
FAVORITE 0 TOTAL DOWNLOAD COUNT 401

0

401

1

298

2

7421

Numerical Analysis of NACA 6409 and Eppler 423 Airfoils
Published: 2023 , Journal of Polytechnic
DOI: 10.2339/politeknik.959517
FAVORITE 2 TOTAL DOWNLOAD COUNT 5400

2

5400

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 2657

0

2657

1

925

Investigation of Wing Forms Through Mass and Wing Area Chart
DOI: 10.46810/tdfd.1084396
FAVORITE 0 TOTAL DOWNLOAD COUNT 1605

0

1605

Investigation of Wing, Fuselage and Tail Design Parameters in Boeing and Airbus Aircraft
DOI: 10.31590/ejosat.1017730
FAVORITE 1 TOTAL DOWNLOAD COUNT 5327

1

5327

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 769

0

769

Effect of Rib Shape on Flow Regime and Heat Transfer
DOI: 10.34248/bsengineering.882373
FAVORITE 0 TOTAL DOWNLOAD COUNT 401

0

401

0

1999

Unpowered Flight Principle: Sailplane
Published: 2019 , Mühendis ve Makina
DOI: -
FAVORITE 0 TOTAL DOWNLOAD COUNT 2304

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2304

Publications

Aerodynamic Performance Comparison of Airfoils in Flying Wing UAV
DOI: 10.46460/ijiea.1169652
CITED 3 FAVORITE 2 TOTAL DOWNLOAD COUNT 7421

3

2

7421

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 769

1

0

769

3

0

1999

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