Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability

For lateral-directional stability analysis, the horizontal tail geometricparameters effect has not been considered. In the present work, the effect ofhorizontal tail aspect ratio on the lateral-directional stability derivatives,rolling static, lateral dynamic stability and Routh discriminate of the...

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Main Author: A.R. Mohammed
Format: Article
Language:English
Published: Unviversity of Technology- Iraq 2007-06-01
Series:Engineering and Technology Journal
Online Access:https://etj.uotechnology.edu.iq/article_181291_448252d53c787e681869ff9d4e2404e6.pdf
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author A.R. Mohammed
author_facet A.R. Mohammed
author_sort A.R. Mohammed
collection DOAJ
description For lateral-directional stability analysis, the horizontal tail geometricparameters effect has not been considered. In the present work, the effect ofhorizontal tail aspect ratio on the lateral-directional stability derivatives,rolling static, lateral dynamic stability and Routh discriminate of the airplaneis investigated.The increasing of the horizontal tail aspect ratio improves both the rollingstatic stability and damping ability in the rolling convergence mode anddecreases the damping ability in spiral mode. The results could be used as realdesign requirements for further configuration improvements of the airplane.
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spelling doaj.art-c1f94ef6bf6549d7a76a5b1cc971dbcc2024-02-04T17:54:42ZengUnviversity of Technology- IraqEngineering and Technology Journal1681-69002412-07582007-06-0125674675610.30684/etj.25.6.5181291Effect of Airplane Tail Aspect Ratio on Lateral- Directional StabilityA.R. MohammedFor lateral-directional stability analysis, the horizontal tail geometricparameters effect has not been considered. In the present work, the effect ofhorizontal tail aspect ratio on the lateral-directional stability derivatives,rolling static, lateral dynamic stability and Routh discriminate of the airplaneis investigated.The increasing of the horizontal tail aspect ratio improves both the rollingstatic stability and damping ability in the rolling convergence mode anddecreases the damping ability in spiral mode. The results could be used as realdesign requirements for further configuration improvements of the airplane.https://etj.uotechnology.edu.iq/article_181291_448252d53c787e681869ff9d4e2404e6.pdf
spellingShingle A.R. Mohammed
Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
Engineering and Technology Journal
title Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
title_full Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
title_fullStr Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
title_full_unstemmed Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
title_short Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability
title_sort effect of airplane tail aspect ratio on lateral directional stability
url https://etj.uotechnology.edu.iq/article_181291_448252d53c787e681869ff9d4e2404e6.pdf
work_keys_str_mv AT armohammed effectofairplanetailaspectratioonlateraldirectionalstability