Search Results - sivaram gogineni

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AC Plasma Anemometer for Hypersonic Mach Number Experiments
Method and system for obtaining flow information, especially useful for high Mach number situations such as:Understand mechanisms of stability and transition to turbulence caused by high speed boundary layerUnderstand high-speed flows in compressors and turbinesUnderstand and monitor combustion instability in gas turbine engines Design supersonic i...
Published: 3/12/2015   |   Inventor(s): Thomas Corke, Eric Matlis, Sivaram Gogineni
Keywords(s):  
Category(s): Manufacturing
AC Plasma Anemometer for Hypersonic Mach Number Experiments
Method and system for obtaining flow information, especially useful for high Mach number situations.
Published: 11/28/2012   |   Inventor(s): Thomas Corke, Eric Matlis, Sivaram Gogineni
Keywords(s):  
Category(s): Devices
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