Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
D. R. Dreim (Northrop Grumman (United States) Falls Church, United States) S. B. Jacobson (Northrop Grumman (United States) Falls Church, United States) R. T Britt (Northrop Grumman (United States) Falls Church, United States) Date Acquired
August 19, 2013
Publication Date
June 1, 1999
Publication Information
Publication: CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
Issue: Pt. 2
Subject Category
Aircraft Design, Testing And Performance Meeting Information
Meeting: CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
Location: Williamsburg, VA
Country: US
Start Date: June 22, 1999
End Date: June 25, 1999
Sponsors: American Institute of Aeronautics and Astronautics, National Aeronautics and Space Administration, Confederation of European Aerospace Societies, Institute for Computer Applications in Science and Engineering
Funding Number(s)
CONTRACT_GRANT: NAS1-19347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Residual pitch oscillationLimit cycle oscillationShock induced oscillationTransonic aerodynamicsBody freedom flutterHump modeComputational fluid dynamicsComputational aeroelasticity