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Application of unsteady aerodynamic methods for transonic aeroelastic analysisAerodynamic methods for aeroelastic analysis are applied to various flow problems. These methods include those that solve the three-dimensional transonic small disturbance (TSD) potential equation, the two-dimensional full potential (FP) equation, and the thin-layer Navier-Stokes equations. Flutter analysis performed using TSD aerodynamics shows that such methods can be used to analyze some aeroelastic phenomena. For thicker bodies and larger amplitude motions a nonisentropic full potential method is presented.
Document ID
19890026210
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitlow, Woodrow, Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Structural Mechanics
Meeting Information
Meeting: ICAS Congress
Location: Jerusalem
Country: Israel
Start Date: August 28, 1988
Sponsors: ICAS
Accession Number
89A13581
Distribution Limits
Public
Copyright
Other

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