Identification of an Unsteady Aerodynamic Model up to High Angle of Attack Regime

Identification of an Unsteady Aerodynamic Model up to High Angle of Attack Regime

The harmonic oscillatory tests for a fighter aircraft configuration using the Dynamic Plunge-Pitch-Roll (DyPPiR) model mount at Virginia Tech Stability Wind Tunnel are described and analyzed. The corresponding data reduction methods are developed on the basis of multirate digital signal processing t...

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Bibliographic Details
Main Author: Fan, Yigang
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Aerodynamic Model
Unsteady Aerodynamic Characteristics
Signal Processing
Parameter Identification
Online Access:http://hdl.handle.net/10919/29830
http://scholar.lib.vt.edu/theses/available/etd-11597-162813/

Internet

http://hdl.handle.net/10919/29830
http://scholar.lib.vt.edu/theses/available/etd-11597-162813/

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