Investigations of Two Wind Turbines in a Row By Using CFD With Actuator Disk Model And Overset Grids

Date

2013-10-04

Author

Türkal, Mert
Novikov, Yaroslav
Üşenmez, Serdar
Sezer Uzol, Nilay
Uzol, Oğuz

Metadata

Show full item record

Item Usage Stats

35
views

0
downloads

URI

https://ruzgem.metu.edu.tr/a/ruzgem-2013-ruzgar-enerjisi-bilim-ve-teknolojileri-konferansi-0
https://hdl.handle.net/11511/71611

Collections

Unverified, Conference / Seminar

Suggestions

OpenMETU
Core

Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile Kahveci, Harika Senem (2021-07-01) One of the challenges in the design of a high-pressure turbine blade is that a considerable amount of cooling is required so that the blade can survive high temperature levels during engine operation. Another challenge is that the addition of cooling should not adversely affect blade aerodynamic performance. The typical flat tips used in designs have evolved into squealer form that implements rims on the tip, which has been reported in several studies to achieve better heat transfer characteristics as well ...
Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile Kahveci, Harika Senem (2020-01-01) One of the challenges in the design of a high-pressure turbine blade is that a considerable amount of cooling is required so that the blade can survive high temperature levels during engine operation. Another challenge is that the addition of cooling should not adversely affect blade aerodynamic performance. Besides, the tip region of a blade is exposed to further complexities due to tip leakage flow that is known to affect flow features and to cause additional pressure losses. The typical flat tips used in...
Investigation of Air Core Characteristics of a Pressure Swirl Injector Using Two Different Volume of Fluid Methods Öztürkmen, Musa Onur; Özyörük, Yusuf (null; 2019-09-20)
Investigation of flowfield characteristics due to shock wave-boundary layer interaction on compression decompression corners using les Karpuzcu, Irmak Taylan; Sert, Cüneyt; Department of Mechanical Engineering (2019) Shock wave boundary layer interactions occur in industrial flows where the flow is transonic, supersonic or hypersonic and there is an incoming boundary layer present. Many of the air crafts such as planes, rockets, missiles, re-entry vehicles, and supersonic wind tunnels experience shock wave boundary layer interactions. These interactions can take place on an air craft at several different places such as the air intakes, ramps, forebody and fins, and also the diffuser section of a supersonic wind tunnel. ...
Investigation of flow around a bridge abutment in a flat bed channel using Large Eddy Simulation Köken, Mete (2007-12-01) Large Eddy Simulation (LES) is used to numerically investigate the horseshoe vortex (HV) system around a vertical bridge abutment located on a flat bed in a straight channel with vertical lateral walls corresponding to conditions at the initiation of the scour process. The simulation is performed with upstream fully turbulent flow including the turbulent fluctuations obtained from a precalculated LES simulation. The dynamics of the instantaneous coherent structures associated with the HV system around the b...

Citation Formats

M. Türkal, Y. Novikov, S. Üşenmez, N. Sezer Uzol, and O. Uzol, “Investigations of Two Wind Turbines in a Row By Using CFD With Actuator Disk Model And Overset Grids,” 2013, Accessed: 00, 2021. [Online]. Available: https://ruzgem.metu.edu.tr/a/ruzgem-2013-ruzgar-enerjisi-bilim-ve-teknolojileri-konferansi-0.