9834301OCR.pdf (534.38 kB)
Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators
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posted on 2018-08-06, 00:00 authored by Mehul Patel, Thomas C. CorkeA method of increasing the performance of an aircraft, missile, munition or ground vehicle with plasma actuators, and more particularly of controlling fluid flow across their surfaces or other surfaces which would benefit from such a method, includes the design of an aerodynamic plasma actuator for the purpose of controlling airflow separation over a control surface of a aircraft, missile, or a ground vehicle, and a method of determining a modulation frequency for the plasma actuator for the purpose of fluid flow control over these vehicles. Various embodiments provide steps to increase the efficiency of aircraft, missiles, munitions and ground vehicles. The method of flow control reduces the power requirements of the aircraft, missile, munition or ground vehicle. These methods also provide alternative aerodynamic control using low-power hingeless plasma actuator devices.
History
Patent Number
US 9,834,301 B1Other Application
13/570,684Inventor
Thomas C. Corke Mehul PatelInventor from Local Institution
Thomas C. CorkeAssignee
University of Notre Dame Du Lac Orbital Research Inc. (Cleveland, OH)Date Modified
2018-08-06Language
- English
Claims
13Publisher
U.S. Patent and Trademark OfficeCooperative Patent Classification Codes
B62D 35/007 (20130101); B64C 23/005 (20130101); F42B 10/40 (20130101); F42B 10/38 (20130101); F42B 10/668 (20130101); Y02T 50/166 (20130101); B64C 2230/12 (20130101)Contributor
Thomas C. CorkeInternational Patent Classification Codes
F42B 10/38 (20060101); B64C 23/00 (20060101); B62D 35/00 (20060101)Usage metrics
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