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Flow and Noise Control: Toward a Closer LinkageMotivated by growing demands for aircraft noise reduction and for revolutionary new aerovehicle concepts, the late twentieth century witnessed the beginning of a shift from single-discipline research, toward an increased emphasis on harnessing the potential of flow and noise control as implemented in a more fully integrated, multidisciplinary framework. At the same time, technologies for developing radically new aerovehicles, which promise quantum leap benefits in cost, safety and performance benefits with environmental friendliness, have appeared on the horizon. Transitioning new technologies to commercial applications will also require coupling further advances in traditional areas of aeronautics with intelligent exploitation of nontraditional and interdisciplinary technologies. Physics-based modeling and simulation are crucial enabling capabilities for synergistic linkage of flow and noise control. In these very fundamental ways, flow and noise control are being driven to be more closely linked during the early design phases of a vehicle concept for optimal and mutual noise and performance benefits.
Document ID
20030014128
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Thomas, Russell H.
(NASA Langley Research Center Hampton, VA United States)
Choudhari, Meelan M.
(NASA Langley Research Center Hampton, VA United States)
Joslin, Ronald D.
(Office of Naval Research Arlington, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 23rd International Council of the Aeronautical Sciences
Location: Toronto
Country: Canada
Start Date: September 8, 2002
End Date: September 13, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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