Now showing items 1-10 of 18
Investigation of Poststall Pitch Oscillations of an Aircraft Wind-Tunnel Model
(American Institute of Aeronautics and Astronautics, AIAA, 2013-08)
A five-degree-of-freedom dynamic wind-tunnel rig is used in the observation of large-amplitude, stall-related and self-sustaining, pitch oscillations of a model aircraft. These oscillations are investigated on the dynamic ...
Aerodynamic model development and simulation of airliner spin for upset recovery
(EDP Sciences, 2013-06)
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of attack, sideslip and angular rate based on experimental data obtained in wind tunnels using static, forced oscillations ...
Investigation of Attainable Equilibrium Sets for Clearance of Flight Control Laws
(American Institute of Aeronautics and Astronautics, AIAA, 2010-01)
A systematic investigation of aircraft equilibrium states and their local stability characteristics is used for clearance of flight control laws for a large variety of manoeuvres. The proposed approach is illustrated by ...
Nonlinear unsteady aerodynmiac modeling by Volterra variational approach
(American Institute of Aeronautics and Astronautics (AIAA), 2012-08)
The aerodynamics at high-angle-of-attack is an unsteady and nonlinear phenomena in time. In this paper, we present a phenomenological and mathematically rigorous approach to nonlinear modeling of the unsteady aerodynamics ...
SUPRA - Enhanced Upset Recovery Simulation
(American Institute of Aeronautics and Astronautics, AIAA, 2012-08)
The SUPRA research project – Simulation of Upset Recovery in Aviation – has been funded by the European Union the Framework Program to enhance the flight simulation envelope for upset recovery simulation. Within the project ...
Aerodynamic model of transport airplane in extended envelope for simulation of upset recovery
(ICAS 2012 CD-ROM PROCEEDINGS, 2012-09)
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with under wing engines and conventional tail developed within the EU Framework Programme (FP7) research project Simulation of ...
A new immersed boundary method for compressible Navier-Stokes equations.
(Taylor and Francis, 2013)
Pushing Ahead - SUPRA Airplane Model for Upset Recovery
(American Institute of Aeronautics and Astronautics, 2012)
One of the primary objectives of the European Union 7th Framework Program research project SUPRA – “Simulation of Upset Recovery in Aviation” – is the development and validation of the aerodynamic model of a generic large ...
Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles
(American Institute of Aeronautics and Astronautics, AIAA, 2011-09)
A five-degree-of-freedom dynamic wind tunnel rig is used in the observation of large amplitude self-sustaining pitch oscillations of a model aircraft. These oscillations arise during a quasi-steady ramp input to the aircraft ...