Flight at high angles of attack is associated with a variety of types of aircraft departure and post stall behaviour. Every aircraft will exhibit specific set of flight characteristics in extended flight envelope. This work was motivated by the need for using flight simulator in training pilots in those high angles of attack conditions to give pilots awareness about nonlinear aircraft behaviours and peculiarities of flight at stall and above stall. Flight simulators, equipped with representative aerodynamic models covering normal and extended flight envelope can be utilised for this purpose. A special approach of building a synthetic aerodynamic model over an available high angle of attack aerodynamic model is discussed in this paper. The ...
Simulation of a dynamic system is known to be sensitive to various factors and one of them could be...
The increasing demand on high performance fighter aircraft has introduced areas of concern associate...
The subject of thepresent thesis is the development of a Flight envelope protection system module to...
The file attached to this record is the author's final peer reviewed version.open access articleThe ...
Loss-of-control following aerodynamic stall remains the largest contributor to fatal civil aviation ...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
The European research project SUPRA (“Simulation of Upset Recovery in Aviation”) produced an extende...
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with und...
Aircraft departing from the nominal flight envelop and entering upset situations have become a major...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
Abstract:Flight simulation now becomes an approach that can effectively and safely be used for engin...
Flight safety of modern transport aviation depends to a large extent on the skills of the pilot in d...
Air carriers will use simulators to train pilots to recover from fully developed stalls. Flight simu...
In recent years, extensive research has been performed in post-stall aerodynamic model development t...
The design of innovative control concepts by using the opportunities of an active high lift system i...
Simulation of a dynamic system is known to be sensitive to various factors and one of them could be...
The increasing demand on high performance fighter aircraft has introduced areas of concern associate...
The subject of thepresent thesis is the development of a Flight envelope protection system module to...
The file attached to this record is the author's final peer reviewed version.open access articleThe ...
Loss-of-control following aerodynamic stall remains the largest contributor to fatal civil aviation ...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
The European research project SUPRA (“Simulation of Upset Recovery in Aviation”) produced an extende...
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with und...
Aircraft departing from the nominal flight envelop and entering upset situations have become a major...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
Abstract:Flight simulation now becomes an approach that can effectively and safely be used for engin...
Flight safety of modern transport aviation depends to a large extent on the skills of the pilot in d...
Air carriers will use simulators to train pilots to recover from fully developed stalls. Flight simu...
In recent years, extensive research has been performed in post-stall aerodynamic model development t...
The design of innovative control concepts by using the opportunities of an active high lift system i...
Simulation of a dynamic system is known to be sensitive to various factors and one of them could be...
The increasing demand on high performance fighter aircraft has introduced areas of concern associate...
The subject of thepresent thesis is the development of a Flight envelope protection system module to...