Now showing items 1-6 of 6
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 ...
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 ...
Analysis of Aircraft Nonlinear Dynamics Using Non-Gradient Based Numerical Methods and Attainable Equilibrium Sets
Multiple equilibrium solutions of aircraft motion equation are investigated using non-gradient based numerical methods and computation of attainable equilibrium sets. The proposed approach may be applied to realistic ...