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Search Results - miguel+visbal
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Linear Plasma Actuator for Dynamic Stall Control
Ionizes and Controls Air Flow to Improve Helicopter Wing Performance This helicopter wing flow control device deploys a plasma actuator with a linear counter-flow point embedded electrode design to force airflow around curved surfaces to counter dynamic stalls. Dynamic stalls occur when a wing loses lift at a high pitch rate. These undesirable events...
Published: 8/28/2024
|
Inventor(s):
Subrata Roy
,
Alexander Lilley
,
Miguel Visbal
Keywords(s):
Category(s):
Technology Classifications > Engineering
,
Technology Classifications > Engineering > Mechanical
,
Technology Classifications > Engineering > Materials