Eksenel kompresörlerin matematik simulasyon yolu ile performanslarının saptanması

Date

1985-08-15

Author

Aksel, M.haluk

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https://hdl.handle.net/11511/95569

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Department of Mechanical Engineering, Project and Design

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Eksenel kompresörler üzerinde deneysel araştırma yapmak için bir deney düzeninin tasarımı, kurulması ve geliştirilmesi Eralp, Cahit O.; Hatip, Etka Ö.(1985)
Eksenel kompresörlerde giriş koşulları ve hava alığının kompresör performansına etkisi üzerinde deneysel bir çalışma Eralp, Cahit O.; Albayrak, Kahraman(1989)
Design, construction and performance evaluation of axial flow fans Keklikoğlu, Hayrettin Özgür; Albayrak, Kahraman; Department of Mechanical Engineering (2019) The primary purposes of this study are to examine the methods used in axial flow fan design, to perform these methods on the design of an axial fan, to develop a design application in order to reduce the design errors and spent time in the design process, and to determine the reliability of the application with numerical and experimental methods. This study is concerned with the design of axial flow fans. It provides detailed information about the design process — additionally, a design code is implemented....
Development of an automatic design and analysis tool for axial compressors Kündeş, Necmettin Anıl; Aksel, Mehmet Haluk; Baran, Özgür Uğraş; Department of Mechanical Engineering (2017) In this thesis, an automatic design and analysis tool is developed for the design of an axial flow compressor and to check the required design conditions of the designed compressor by using three dimensional CFD analyses automatically. The developed tool mainly consists of six parts which are mean line design, calculations based on radial equilibrium theory, parametrization, generation of three dimensional blade geometry, mesh generation and solver. A new design study for an axial flow compressor begins wit...
Development of an axisymmetric, turbulent and unstructured navier-stokes solver Akdemir, Mustafa; Aksel, Mehmet Haluk; Department of Mechanical Engineering (2010) An axisymmetric, Navier-Stokes finite volume flow solver, which uses Harten, Lax and van Leer (HLL) and Harten, Lax and van Leer–Contact (HLLC) upwind flux differencing scheme for spatial and uses Runge-Kutta explicit multi-stage time stepping scheme for temporal discretization on unstructured meshe is developed. Developed solver can solve the compressible axisymmetric flow. The spatial accuracy of the solver can be first or second order accurate. Second order accuracy is achieved by piecewise linear recons...

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M. h. Aksel, “Eksenel kompresörlerin matematik simulasyon yolu ile performanslarının saptanması,” 1985. Accessed: 00, 2022. [Online]. Available: https://hdl.handle.net/11511/95569.