Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter

An edition of Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter (1992)

Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter

By Aparajit J. Mahajan

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Publish Date

1992

Publisher

National Aeronautics and Space Administration,For sale by the National Technical Information Service

Language

eng

Pages

Description:

subjects: Aeroelasticity, Flutter (Aerodynamics)