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Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches

Summary in English.

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Bibliographic Details
Main Author: Pienaar, D van V
Other Authors: Redelinghuys, Christiaan
Format: Thesis
Language:English
Published: Department of Mechanical Engineering 2014
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access_status_str Open Access
author Pienaar, D van V
author2 Redelinghuys, Christiaan
author_browse Pienaar, D van V
Redelinghuys, Christiaan
author_facet Redelinghuys, Christiaan
Pienaar, D van V
author_sort Pienaar, D van V
collection Thesis
description Summary in English.
format Thesis
id oai:open.uct.ac.za:11427/5486
institution University of Cape Town (South Africa)
language eng
last_indexed 2026-06-10T12:33:37.862Z
license_str Not specified — see source repository
provenance_str_mv Harvested via OAI-PMH from UCTD — University of Cape Town Open Access Repository
publishDate 2014
publishDateRange 2014
publishDateSort 2014
publisher Department of Mechanical Engineering
publisherStr Department of Mechanical Engineering
record_format dspace
source_str UCTD — University of Cape Town Open Access Repository
spelling oai:open.uct.ac.za:11427/5486 Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches Pienaar, D van V Redelinghuys, Christiaan Mechanical Engineering Summary in English. The investigation of the stability of longitudinal motion of fixed wing aircraft in ground proximity presented here focuses on rectangular wing and tail configurations similar to that of the Piper Cherokee PA-28-180. The majority of our results pertain to the height range down to one quarter of the wing span, and th main objectives of the investigation were the following: to reveal the physical nature and causes of the instability encountered in the close ground proximity; to assess the influence the design parameters such as the centre of the mass placement, tail length, tail height and wing aspect ration have on the stability of longitudinal motion; and to suggest a feedback control strategy that would alleviate the instability. 2014-07-31T11:19:05Z 2014-07-31T11:19:05Z 2000 Doctoral Thesis Doctoral PhD http://hdl.handle.net/11427/5486 eng application/pdf Department of Mechanical Engineering Faculty of Engineering and the Built Environment University of Cape Town
spellingShingle Mechanical Engineering
Pienaar, D van V
Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
thesis_degree_str Doctoral
title Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
title_full Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
title_fullStr Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
title_full_unstemmed Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
title_short Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
title_sort longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches
topic Mechanical Engineering
url http://hdl.handle.net/11427/5486
work_keys_str_mv AT pienaardvanv longitudinalstabilityandcontrolanalysisandparametersensitivityinvestigationoffixedwingaircraftingroundproximityusingvariousaerodynamicapproaches