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Snapshot of Active Flow Control Research at NASA LangleyNASA Langley is aggressively investigating the potential advantages of active flow control as opposed to more traditional aerodynamic techniques. Many of these techniques will be blended with advanced materials and structures to further enhance payoff. Therefore a multi-disciplinary approach to technology development is being attempted that includes researchers from the more historical disciplines of fluid mechanics. acoustics, material science, structural mechanics, and control theory. The overall goals of the topics presented are focused on advancing the state of knowledge and understanding of controllable fundamental mechanisms in fluids rather than on specific engineering problems. An organizational view of current research activities at NASA Langley in active flow control as supported by several programs such as the Morphing Project under Breakthrough Vehicle Technologies Program (BVT). the Ultra-Efficient Engine Technology Program (UEET), and the 21st Century Aircraft Technology Program (TCAT) 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, as part of the fundamental NASA R and D (research and development) program. will be demonstrated as either bench-top experiments, wind-tunnel investigations, or in flight tests. Later they will be transferred to more applied research programs within NASA, DOD (Department of Defense), and U.S. industry.
Document ID
20030000830
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Washburn, A. E.
(NASA Langley Research Center Hampton, VA United States)
Gorton, S. Althoff
(NASA Langley Research Center Hampton, VA United States)
Anders, S. G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2002-3155
Report Number: AIAA Paper 2002-3155
Meeting Information
Meeting: 1st 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.
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