Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification

Author:

Pattinson J.1,Lowenberg M. H.1,Goman M. G.2

Affiliation:

1. Department of Aerospace Engineering, University of Bristol, Bristol, England BS8 1TR, United Kingdom

2. Department of Engineering, De Montfort University, Leicester, England LE1 9BH, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference50 articles.

1. CosentinoG. B. “Computational Fluid Dynamics Analysis Success Stories of X-Plane Design to Flight Test,” NASA TM 2008-214636, May 2008.

2. TobakM.SchiffL. “On the Formulation of the Aerodynamic Characteristics in Aircraft Dynamics,” NASA TR 456, 1976.

3. “Cooperative Programme on Dynamic Wind Tunnel Experiments for Manoeuvring Aircraft,” AGARD Rept. AR-305, Oct. 1996.

4. Aircraft Stability and Control Characteristics Determined by System Identification of CFD Simulations

5. Evaluation of a Three Degree of Freedom Test Rig for Stability Derivative Estimation

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