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Active Flow Control Activities at NASA LangleyNASA Langley continues to aggressively investigate the potential advantages of active flow control over more traditional aerodynamic techniques. This paper provides an update to a previous paper and describes both the progress in the various research areas and the significant changes in the NASA research programs. The goals of the topics presented are focused on advancing the state of knowledge and understanding of controllable fundamental mechanisms in fluids as well as to address engineering challenges. An organizational view of current research activities at NASA Langley in active flow control as supported by several projects is presented. On-center research as well as NASA Langley funded contracts and grants are discussed at a relatively high level. The products of this research are to be demonstrated either in bench-top experiments, wind-tunnel investigations, or in flight as part of the fundamental NASA R&D program and then transferred to more applied research programs within NASA, DOD, and U.S. industry.
Document ID
20040084677
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Anders, Scott G.
(NASA Langley Research Center Hampton, VA, United States)
Sellers, William L., III
(NASA Langley Research Center Hampton, VA, United States)
Washburn, Anthony E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2004-2623
Report Number: AIAA Paper 2004-2623
Meeting Information
Meeting: 2nd AIAA Flow Control Conference
Location: Portland, OR
Country: United States
Start Date: June 28, 2004
End Date: July 1, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-762-55-MF
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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