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Aeroelastic Analysis for Aeropropulsion ApplicationsAeroelastic codes with advanced capabilities for modeling flow require substantial computational time. On the other hand, fast-running linear aeroelastic codes lack the capability to model three-dimensional, transonic, vortical, and viscous flows. The goal of this work was to develop an aeroelastic code with accurate modeling capabilities and small computational requirements.
Document ID
20020034911
Acquisition Source
Glenn Research Center
Document Type
Contractor or Grantee Report
Authors
Keith, Theo G., Jr. (Toledo Univ. OH United States)
Bakhle, Milind A. (Toledo Univ. OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NCC3-527
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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