Axial flow compressor aerodynamic design and analysis

Download
007317.pdf
1989
Çakıroğlu, Mahir
Show full item record
232
views
0
downloads
https://hdl.handle.net/11511/6219
Graduate School of Natural and Applied Sciences, Thesis

Suggestions

Axial compressor and turbine stage design using through-flow and blade-to-blade codes
Gönç, L. Oktay; Üçer, Ahmet Ş.; Department of Mechanical Engineering (1998)
Thrust vector control of a rocket vehicle associated with aerodynamic control
Kaya, Cumhur Yalçın; Özgören, M. Kemal; Department of Mechanical Engineering (1989)
Vortex flow aerodynamics behind a symmetric airfoil at low angles of attack and Reynolds numbers
Kurtuluş, Dilek Funda (2021-11-01)
The low Reynolds number aerodynamics is important to investigate for micro air vehicle applications. The current paper covers numerical simulations to present the downstream development of the wake patterns and detailed analysis of the vortices generated at the downstream of NACA 0012 airfoil around the critical angle of attack where the instantaneous vortex patterns are oscillatory and differ from the mean vortex pattern for low Reynolds numbers ranging from 1000 to 4000. The instantaneous and mean aerodyn...
Aerodynamic Loads of Small-Amplitude Pitching NACA 0012 Airfoil at Reynolds Number of 1000
Kurtuluş, Dilek Funda (2018-08-01)
Aerodynamic Analyses of Thick Wind Turbine Airfoils for High Reynolds Numbers
ASLAN, EZGİ; Orbay Akcengiz, Ezgi; Sezer Uzol, Nilay (2021-09-08)
In this study, Computational Fluid Dynamics simulations of flow around thick have been performed. Thick airfoils are generally preferred in wind turbine blades for structural and aerodynamic performances. High Reynolds flows around thick airfoils are one of the challenging problems in wind turbine blade design due to turbulent, separated and complex flow field characteristics. In the CFD analyses, both 2-D RANS simulation approach on structured computational grids is considered. Grid sensitivity study is al...
Citation Formats
M. Çakıroğlu, “Axial flow compressor aerodynamic design and analysis,” Middle East Technical University, 1989.
METU IIS - Integrated Information Service open@metu.edu.tr