Estimation of aircraft nonlinear unsteady parameters from wind tunnel data

An edition of Estimation of aircraft nonlinear unsteady parameters from wind tunnel data (1998)

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data

By Vladislav Klein

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Publish Date

1998

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Aerodynamic forces, Aircraft stability, Flight stability tests, Mathematical models, Unsteady aerodynamics, Wind tunnel tests