An analysis of the flight dynamics of a second generation SST aircraft

Show simple item record Steer, Anthony J. en_UK 1999 en_UK 2005-11-23T12:20:19Z 2005-11-23T12:20:19Z 1999 en_UK
dc.description.abstract This interim report covers an initial overview of delta-wing aircraft static, dynamic and control characteristics, collated from publications within the public domain and the authors related research. This is to give the reader an overall understanding how a delta-winged supersonic transport aircraft’ s characteristics differ to those of a conventional civil transport aircraft. This is followed by identifying the aircraft’s static and dynamic stability, with the effect of speed and CG location on the aircraft dynamic modes specifically addressed. Following this, a comprehensive investigation and analysis of the open loop response of a SCT baseline aircraft, in both low-speed cruise and approach and landing conditions, has been carried out. Both time and frequency domain techniques have been utilised. Finally, conclusions are made based on the results of the work presented. en_UK
dc.description.sponsorship Cranfield University en_UK
dc.format.extent 1963 bytes
dc.format.extent 3450779 bytes
dc.format.mimetype text/plain
dc.format.mimetype application/pdf
dc.language.iso en_UK en_UK
dc.relation.ispartofseries College of Aeronautics Report;9914 en_UK
dc.relation.ispartofseries CU/CoA;9914 en_UK
dc.title An analysis of the flight dynamics of a second generation SST aircraft en_UK
dc.type Technical Report en_UK

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