5-Degree-of-Freedom Dynamic Rig for Wind Tunnel Tests of Aerospace Vehicles
Authors:
- 14 June 2009
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Investigation of a Half-Model High-Lift Configuration in a Wind TunnelJournal of Aircraft, 2008
- Wind-Tunnel Measurements of the E-8C Modeled with and Without WingletsJournal of Aircraft, 2008
- Reduced-Frequency Approach for Calculating Dynamic DerivativesAIAA Journal, 2007
- Birth of Sweepback: Related Research at Luftfahrtforschungsanstalt-GermanyJournal of Aircraft, 2005
- Validation of Methodology for Estimating Aircraft Unsteady Aerodynamic Parameters from Dynamic Wind Tunnel Tests2003
- Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus2002
- Implications of Recent Rotary Rig Results for Flight PredictionJournal of Aircraft, 2000
- Wind-Tunnel Aerodynamics in Rotary Tests of Combat Aircraft ModelsJournal of Aircraft, 1998
- Nonlinear command augmentation system for a high performance aircraft1993
- 1986-A Year For Filling In the SpacesJournal of Aircraft, 1986