Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
Book Description
Numerical Investigation of Flow Maldistribution and Pressure Losses Reduction in 3D Turning Diffusers by Means of Varying Area Ratios
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
Book Description
Experimental Investigation of Flow Maldistribution and Pressure Losses Reduction in 3D Turning Diffusers by Means of Varying Area Ratios
Author:
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 82
Book Description
Numerical Investigation of Flow Maldistribution and Pressure Losses in Turning Diffusers by Means of Installing Baffles
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Numerical Investigation of Flow Through Wide Angle Diffusers
Author: Moududur Rahman
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 258
Book Description
This study is aimed at the development of a computational technique for the prediction of the flow field in wide angle diffusers. The finite element technique is used for the solution of the governing equations. A commercial software package, NISA/3DFlUID, modified for this specific application was used. The parameters affecting the flow field have been identified. For a wide range of variation of these parameters, the effects on the flow field have been examined. This investigation is an exhaustive and comprehensive numerical study of diffuser flows. Such a study will result in substantial improvement in the understanding of the anatomy of the flow field. The creation of the current knowledge base will also enable a judicious selection of diffusers for industrial applications. It was found that for laminar flow through wide angle diffusers the computational technique adequately predicted the qualitative and quantitative behavior of the flow field. Therefore new results, as predicted by the current computational technique have been presented. For example, it was found that the effective recirculation length varies exponentially with the angle of expansion of the diffuser. For turbulent flow the standard k-e model has been found to be qualitatively adequate in representing the flow field. However, the quantitative predictions are being compared with available experimental results and those obtained using other numerical schemes. A wide range of possibilities exist for the constants and boundary conditions employed in k-e modeling. Such a numerical experimentation requires deep understanding of the equations governing the flow field. The validity and/or adjustments of these constants and boundary conditions for diffuser flow are investigated.
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 258
Book Description
This study is aimed at the development of a computational technique for the prediction of the flow field in wide angle diffusers. The finite element technique is used for the solution of the governing equations. A commercial software package, NISA/3DFlUID, modified for this specific application was used. The parameters affecting the flow field have been identified. For a wide range of variation of these parameters, the effects on the flow field have been examined. This investigation is an exhaustive and comprehensive numerical study of diffuser flows. Such a study will result in substantial improvement in the understanding of the anatomy of the flow field. The creation of the current knowledge base will also enable a judicious selection of diffusers for industrial applications. It was found that for laminar flow through wide angle diffusers the computational technique adequately predicted the qualitative and quantitative behavior of the flow field. Therefore new results, as predicted by the current computational technique have been presented. For example, it was found that the effective recirculation length varies exponentially with the angle of expansion of the diffuser. For turbulent flow the standard k-e model has been found to be qualitatively adequate in representing the flow field. However, the quantitative predictions are being compared with available experimental results and those obtained using other numerical schemes. A wide range of possibilities exist for the constants and boundary conditions employed in k-e modeling. Such a numerical experimentation requires deep understanding of the equations governing the flow field. The validity and/or adjustments of these constants and boundary conditions for diffuser flow are investigated.
A Numerical Investigation of Flow in Rotating Radial Diffusers
Author: A. K. Majumdar
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Water Tunnel Diffuser Flow Studies: Experimental research
Author: Pennsylvania State College. Ordnance Research Laboratory
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 74
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 74
Book Description
Turbomachinery Diffuser Design Technology
Author: David Japikse
Publisher: Concepts Eti
ISBN:
Category : Science
Languages : en
Pages : 312
Book Description
Publisher: Concepts Eti
ISBN:
Category : Science
Languages : en
Pages : 312
Book Description
Experimental and Numerical Investigation of Separated Flow in a Two-dimensional Diffuser
Author: Wisith Jeangprajak
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 176
Book Description
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 176
Book Description
Performance and Flow Regimes in Plane 2-D Diffusers with Exit Channels at Low Reynolds Numbers
Author: Epameinondas Trivilos
Publisher:
ISBN: 9781423500582
Category :
Languages : en
Pages : 99
Book Description
A numerical study on laminar incompressible flows in 2-D straight walled diffusers in the low Reynolds number regime (105-1048) is presented to investigate performance and various flow regimes that might exist. Tail channels are situated downstream the diffusers. Geometries with area ratios AR-=1.15 to 5 and non-dimensional lengths of L/W1=1 to 48 are considered. Results are presented in terms of flow regime maps for Reynolds numbers of 105, 210, 314, 420, 629, 1,048 and pressure recovery coefficients maps for Re numbers of 105, 210, 314, 420 and 629. In addition time resolved simulations of impulsively starting flow are considered at Re=210, 314 for 12 geometries on the flow regime map. Four flow regimes can be distinguished depending on diffuser geometry. With increasing divergence angle the flow goes from attached to symmetrically separated to asymmetrically separated and finally to a non 2-D pattern respectively.
Publisher:
ISBN: 9781423500582
Category :
Languages : en
Pages : 99
Book Description
A numerical study on laminar incompressible flows in 2-D straight walled diffusers in the low Reynolds number regime (105-1048) is presented to investigate performance and various flow regimes that might exist. Tail channels are situated downstream the diffusers. Geometries with area ratios AR-=1.15 to 5 and non-dimensional lengths of L/W1=1 to 48 are considered. Results are presented in terms of flow regime maps for Reynolds numbers of 105, 210, 314, 420, 629, 1,048 and pressure recovery coefficients maps for Re numbers of 105, 210, 314, 420 and 629. In addition time resolved simulations of impulsively starting flow are considered at Re=210, 314 for 12 geometries on the flow regime map. Four flow regimes can be distinguished depending on diffuser geometry. With increasing divergence angle the flow goes from attached to symmetrically separated to asymmetrically separated and finally to a non 2-D pattern respectively.
Computation of Straight Diffusers at Low Mach Number Incorporating an Improved Correlation for Turbulent Detachment and Reattachment
Author: Juan Bardina
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 188
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 188
Book Description