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
Download 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 full books in PDF, epub, and Kindle. Read online free 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 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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 I: Flow at the Exit of Turbine Book in PDF, Epub and Kindle
Presented at the International Gas Turbine and Aeroengine Congress & Exposition, Houston, Texas - June 5-8, 1995.
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.
Author | : |
Publisher | : |
Total Pages | : 1060 |
Release | : 1997 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 536 |
Release | : 1996 |
Genre | : Mechanical engineering |
ISBN | : |
Download Paper Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 572 |
Release | : 1996 |
Genre | : Mechanical engineering |
ISBN | : |
Download ASME Technical Papers Book in PDF, Epub and Kindle
Author | : Upendra S. Rohatgi |
Publisher | : |
Total Pages | : 722 |
Release | : 2002 |
Genre | : Fluid mechanics |
ISBN | : 9780791836163 |
Download Proceedings of the 2002 ASME Joint U.S.-European Fluids Engineering Conference Book in PDF, Epub and Kindle
Author | : B. V. Marathe |
Publisher | : |
Total Pages | : 0 |
Release | : 1994 |
Genre | : |
ISBN | : |
Download Experimental and Numerical Investigation of Stator Exit Flow Field of an Automotive Torque Converter Book in PDF, Epub and Kindle
Presented at the International Gas Turbine and Aeroengine Congress and Exposition, The Hague, Netherlands, June 13-16, 1994.
Author | : M. Zaccaria |
Publisher | : |
Total Pages | : 394 |
Release | : 1997 |
Genre | : Turbines |
ISBN | : |
Download An Experimental Investigation of Steady and Unsteady Flow Field in an Axial Flow Turbine Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 222 |
Release | : 2001 |
Genre | : Fluid mechanics |
ISBN | : |
Download Fluid Power Systems and Technology Book in PDF, Epub and Kindle
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 386 |
Release | : 2018-07-23 |
Genre | : |
ISBN | : 9781723515354 |
Download An Experimental Investigation of Steady and Unsteady Flow Field in an Axial Flow Turbine Book in PDF, Epub and Kindle
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...