FUN3D Analyses in Support of the First Aeroelastic Prediction Workshop

Author:

Chwalowski Pawel1,Heeg Jennifer1

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. 1Yates,C.E.,Land,N.S.,andFoughner,J.T.“MeasuredandCalculatedSubsonicandTransonicFlutterCharacteristicsofa45degSwept-backWingPlanforminAirandinFreon-12intheLangleyTransonicDynamicsTunnel,”NASATechnicalNoteD-1616,March1963.

2. 2Yates,C.E.“AGARDStandardAeroelasticConfigurationsforDynamicResponse-Wing445.6,”AGARDReportNo.765,July1988.

3. 3Bennett,R.M.andEdwards,J.W.“AnOverviewofRecentDevelopmentsinComputationalAeroelasticity,”AIAAPaper1998-2421,June 1998.

4. 6Ricketts,R.H.,Sandford,M.C.,Watson,J.J.,andSeidel,D.A.“GeometricandStructuralPropertiesofaRectangularSupercriticalWing OscillatedinPitchforMeasurementofUnsteadyTrnasonicPressureDistributions,”NASATM1983-85763,Nov.1983.

5. 7Ricketts, R. H., Sandford, M. C., Seidel, D. A., and Watson, J. J. “Transonic Pressure Distributions on a Rectangular Supercritical Wing OscillatinginPitch,”NASATM1983-84616‘,March1983.

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