Zobrazeno 1 - 10
of 74
pro vyhledávání: '"A. Mirzamoghadam"'
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique
Autor:
Ardeshir Riahi, Chao-Cheng Shiau, İzzet Şahin, Izhar Ullah, Je-Chin Han, Alexander V. Mirzamoghadam, Curtis K. Stimpson
Publikováno v:
Journal of Turbomachinery. 142
This work focuses on the parametric study of film cooling effectiveness on the turbine vane endwall under various flow conditions. The experiments were performed in a five-vane annular sector cascade facility in a blowdown wind tunnel. The controlled
Autor:
Chao-Cheng Shiau, Je-Chin Han, Ardeshir Riahi, Alexander V. Mirzamoghadam, Nafiz H. K. Chowdhury
Publikováno v:
Journal of Thermophysics and Heat Transfer. 32:637-647
This work focuses on the parametric experimental study of film cooling effectiveness on the suction side of a scaled turbine vane. The experiments are performed in a five-vane annular sector cascad...
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Autor:
Ardeshir Riahi, Izhar Ullah, Je-Chin Han, Curtis K. Stimpson, Alexander V. Mirzamoghadam, Chao-Cheng Shiau, İzzet Şahin
Publikováno v:
Volume 5B: Heat Transfer.
This work focuses on the parametric study of film cooling effectiveness on turbine vane endwall under various flow conditions. The experiments were performed in a five-vane annular sector cascade facility in a blowdown wind tunnel. The controlled exi
Publikováno v:
Volume 5B: Heat Transfer.
Labyrinth seal designs for reduced leakage have been analyzed by three-dimensional CFD simulations. The objective is to learn the effect of seal geometry modifications on total leakage through the seal and arrive at an advanced seal setting for impro
Publikováno v:
Volume 5B: Heat Transfer.
The interaction between the mainstream and disc cavity purge flows in a turbine stage is an unsteady 360° phenomenon. Most of the current rotating rigs have used steady pressure transducers to measure the mainstream annulus pressure distributions as
Publikováno v:
Volume 5B: Heat Transfer.
This paper is a continuation of a previous comparison dealing with URANS-based validation of the ASU-Honeywell turbine stage mainstream/disc-cavity interaction rig data. Here, the validation is with a CFD code named PowerFLOW which is based on the La
Autor:
Chao-Cheng Shiau, Alexander V. Mirzamoghadam, Ardeshir Riahi, Nafiz H. K. Chowdhury, Je-Chin Han
Publikováno v:
Volume 5C: Heat Transfer.
This work focuses on the parametric experimental study of film cooling effectiveness on the suction side of a scaled turbine vane under transonic flow condition. The experiments were performed in a five-vane annular sector cascade blowdown facility.
Publikováno v:
Volume 5B: Heat Transfer.
The objective of this study is to develop a Computational Fluid Dynamics (CFD) based methodology for analyzing and predicting leakage of worn or rub-intended labyrinth seals during operation. The simulations include intended tooth axial offset and nu
Publikováno v:
Volume 5B: Heat Transfer.
Modeling of hot gas ingestion in a gas turbine engine is critical because its accuracy directly affects performance as well as turbine durability. In this paper, ASU ingestion test rig data accompanied by its published ingress/egress discharge coeffi