Flight control system damage simulation using freely flying models

Flight control system damage simulation using freely flying models

This article deals with a damage simulation of flight control systems during a flight. As a subject of flight tests the model of a classic aerodynamic aircraft scheme is considered. This aircraft has highly swept wings a moderate wing elongation and all-moving horizontal tail surfaces. The diagrams...

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Veröffentlicht in:Aeronautical journal 2005-01, Vol.109 (1091), p.45-50
Hauptverfasser: Sadovnychiy, S., Ryzhenko, A., Betin, A.
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Sprache:eng
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Air transportation and traffic
Applied sciences
Exact sciences and technology
Ground, air and sea transportation, marine construction
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container_issue 1091
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container_title Aeronautical journal
container_volume 109
creator Sadovnychiy, S.
Ryzhenko, A.
Betin, A.
description This article deals with a damage simulation of flight control systems during a flight. As a subject of flight tests the model of a classic aerodynamic aircraft scheme is considered. This aircraft has highly swept wings a moderate wing elongation and all-moving horizontal tail surfaces. The diagrams of flight parameters from flight tests of the freely flying models with loss of a control surface in flight are given. The investigation results for the failures leading to a sharp drop in the stiffness of the control units in the pitch channel are given. The damage investigation in horizontal flight and in complex manoeuvres is given.
doi_str_mv 10.1017/S000192400000052X
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source Cambridge University Press Journals Complete
subjects Air transportation and traffic
Applied sciences
Exact sciences and technology
Ground, air and sea transportation, marine construction
title Flight control system damage simulation using freely flying models
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