Yusuf Özyörük

E-mail

ozyoruk@metu.edu.tr

Department

Department of Aerospace Engineering

ORCID

0000-0001-9944-2826

Scopus Author ID

6602100734

Web of Science Researcher ID

ABD-7117-2020

EFFECTS OF THE REACTION MECHANISM ON HEAT RELEASE FOR THE PREDICTION OF THERMOACOUSTIC INSTABILITIES IN LIQUID ROCKET ENGINES Öztürkmen, Musa Onur; Özyörük, Yusuf (2023-09-13)
NUMERICAL INVESTIGATION OF GENERALIZED K-W TURBULENCE MODEL FOR COMPRESSIBLE DUCT FLOWS YAHŞİ, ÖMER FARUK; Yılmaz, Mehmet H.; Özyörük, Yusuf; Günaydınlıoğlu, Erkan (2023-09-13)
AERODYNAMIC OPTIMIZATION OF INLET DESIGN FOR HIGH BYPASS RATIO TURBOFAN KAPLAN, YAĞIZ; Özyörük, Yusuf (2023-09-13)
Stability Characteristics of a Single Injector Combustor through Acoustic Solutions with Large Eddy Simulated Heat Sources Öztürkmen, Musa Onur; Özyörük, Yusuf (2023-07-09)
Numerical Optimization of High Convoluted Serpentine Air Inlet Duct Using Response Surface Methodology YAHŞİ, ÖMER FARUK; Yılmaz, Mehmet H.; Günaydınlıoğlu, Erkan; Özyörük, Yusuf (2023-06-12)
Investigation of a Solution Approach to Quadratic Eigenvalue Problem for Thermoacoustic Instabilities Öztürkmen, Musa Onur; Özyörük, Yusuf (2022-01-01) © 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.The interactions between the unsteady heat release and pressure fluctuations in a combustion chamber may lead to thermoacoustic instabili...
Transitional DDES Study over a Circular Cylinder and an Airfoil YALÇIN, ÖZGÜR; Cengiz, Kenan; Wein, Lars; Özyörük, Yusuf; Seume, J.R. (2021-09-15)
PREDICTION OF LINEAR COMBUSTION INSTABILITIES IN ROCKET ENGINES, Öztürkmen, Musa Onur; Özyörük, Yusuf (2021-09-01)
Delayed Detached-Eddy Simulations of Transonic Cavity Noise Yalçın, Özgür; Özyörük, Yusuf (2021-08-02) In this paper, computations of transonic (M=0.85) flow over an open cavity are performed through use of a high-order solver employing different Delayed Detached-Eddy Simulation (DDES) strategies: DDES, DDES with shear-laye...
Conjugate Analysis of Silica-Phenolic Charring Ablation Coupled with Interior Ballistics Alanyalioglu, Cetin Ozan; Özyörük, Yusuf (2021-07-01) Because of its excellent insulation capability, the usage of a silica-phenolic charring ablator as a nozzle liner is a common practice in the solid rocket motor industry. During the design of a solid rocket motor employing...

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