A flight simulation study of the handling characteristics of a slender wing supersonic transport aircraft at landing approach speeds

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dc.contributor.author D. H. Perry en_US
dc.contributor.author A. McPherson en_US
dc.date.accessioned 2014-10-21T15:50:09Z
dc.date.available 2014-10-21T15:50:09Z
dc.date.issued 1966 en_US
dc.identifier.other ARC/R&M-3616 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/2884
dc.description.abstract A ground based flight simulator has been used for piloting assessments of the handling characteristics of a slender wing supersonic transport aircraft during the landing approach. The simulation included two methods of representing the outside visual world, and, for some of the tests, cockpit motion in pitch and roll was also used. Amongst the topics studied were the effects of turbulence, and the improvements in handling which could be brought about by autostabilization. Data is presented in the form of pilots' assessments on an opinion rating scale, measurements of the accuracy of performing landing approaches, and time histories of control usage and aircraft response. A brief comparison of these handling assessments with the predictions of existing handling qualities criteria has also been made. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title A flight simulation study of the handling characteristics of a slender wing supersonic transport aircraft at landing approach speeds en_US


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