Experimental Investigation of Steady and Unsteady Flow Field Downstream of an Automotive Torque Converter Turbine and Inside the Stator Part I: Flow at the Exit of Turbine

Experimental Investigation of Steady and Unsteady Flow Field Downstream of an Automotive Torque Converter Turbine and Inside the Stator Part I: Flow at the Exit of Turbine
Author: B. V. Marathe
Publisher:
Total Pages: 0
Release: 1995
Genre:
ISBN:

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Presented at the International Gas Turbine and Aeroengine Congress & Exposition, Houston, Texas - June 5-8, 1995.

Experimental Investigation of Steady and Unsteady Flow Field Downstream of an Automotive Torque Converter Turbine and Inside the Stator Part-II: Unsteady Pressure on The...

Experimental Investigation of Steady and Unsteady Flow Field Downstream of an Automotive Torque Converter Turbine and Inside the Stator Part-II: Unsteady Pressure on The...
Author: B. V. Marathe
Publisher:
Total Pages: 0
Release: 1995
Genre:
ISBN:

Download Experimental Investigation of Steady and Unsteady Flow Field Downstream of an Automotive Torque Converter Turbine and Inside the Stator Part-II: Unsteady Pressure on The... Book in PDF, Epub and Kindle

Presented at the International Gas Turbine and Aeroengine Congress & Exposition, Houston, Texas - June 5-8, 1995.

Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 1060
Release: 1997
Genre: Mechanics, Applied
ISBN:

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Paper

Paper
Author:
Publisher:
Total Pages: 536
Release: 1996
Genre: Mechanical engineering
ISBN:

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ASME Technical Papers

ASME Technical Papers
Author:
Publisher:
Total Pages: 572
Release: 1996
Genre: Mechanical engineering
ISBN:

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An Experimental Investigation of Steady and Unsteady Flow Field in an Axial Flow Turbine

An Experimental Investigation of Steady and Unsteady Flow Field in an Axial Flow Turbine
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 386
Release: 2018-07-23
Genre:
ISBN: 9781723515354

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Measurements were made in a large scale single stage turbine facility. Within the nozzle passage measurements were made using a five hole probe, a two-component Laser Doppler Velocimeter (LDV), and a single sensor hot wire probe. These measurements showed weak secondary flows at midchord, and two secondary flow loss cores at the nozzle exit. The casing vortex loss core was the larger of the two. At the exit radial inward flow was found over the entire passage, and was more pronounced in the wake. Nozzle wake decay was found to be more rapid than for an isolated vane row due to the rotor's presence. The midspan rotor flow field was measured using a two-component LDV. Measurements were made from upstream of the rotor to a chord behind the rotor. The distortion of the nozzle wake as it passed through the rotor blade row was determined. The unsteadiness in the rotor flow field was determined. The decay of the rotor wake was also characterized. Zaccaria, M. and Lakshminarayana, B. Glenn Research Center NASA-CR-4778, NAS 1.26:4778, E-10771 NAG3-555; RTOP 523-26-33...