AC Plasma Anemometer for Hypersonic Mach Number Experiments

Description:

Method and system for obtaining flow information, especially useful for high Mach number situations.

Patent Information:
Category(s):
Devices
For Information, Contact:
Tim Joyce PH
Licensing Associate
University of Notre Dame
 
Inventors:
Thomas Corke
Eric Matlis
Sivaram Gogineni
Keywords:
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