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Overview of Active Flow Control Actuator Development at NASA Langley Research CenterThe paper provides an overview of the actuator development work that is currently underway at NASA Langley Research Center in the context of some of the Active Flow Control research being conducted at NASA Langley. The actuator development effort has provided a focused, centralized location for this work within NASA Langley. The multidisciplinary team approach utilized in this effort has allowed input from multiple disciplines on how various actuator challenges can be addressed and has lead to some unique approaches in actuation.
Document ID
20030006461
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Schaeffler, Norman W.
(NASA Langley Research Center Hampton, VA United States)
Hepner, Timothy E.
(NASA Langley Research Center Hampton, VA United States)
Jones, Gregory S.
(NASA Langley Research Center Hampton, VA United States)
Kegerise, Michael A.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 2002-3159
Report Number: AIAA Paper 2002-3159
Meeting Information
Meeting: 1st AIAA Flow Control Conference
Location: Saint Louis, MO
Country: United States
Start Date: June 24, 2002
End Date: June 26, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available