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Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf

The objective of this project is to do preliminary design of 19 passengers multipurpose airplane. The airplane configuration consists of high wing, two turboprop engines, conventional tail and non-retractable tricycle landing gear. The airplane is designed according FAR 23 regulation. The aircraft o...

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Main Author: Abdul Rauf, Mohd Taha
Format: Thesis
Language:English
Published: 2002
Online Access:https://ir.uitm.edu.my/id/eprint/73890/1/73890.pdf
https://ir.uitm.edu.my/id/eprint/73890/
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spelling my.uitm.ir.738902024-05-21T09:32:44Z https://ir.uitm.edu.my/id/eprint/73890/ Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf Abdul Rauf, Mohd Taha The objective of this project is to do preliminary design of 19 passengers multipurpose airplane. The airplane configuration consists of high wing, two turboprop engines, conventional tail and non-retractable tricycle landing gear. The airplane is designed according FAR 23 regulation. The aircraft operates at the rural to urban area. The analysis involves parametric sizing, undercarriage layout, weight and balance, stability in static longitudinal and flight performance. It is shown that the airplane is stable (static longitudinal) by having negative C ma. In the end, the design requirement and actual perform will be compared. 2002 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/73890/1/73890.pdf Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf. (2002) Degree thesis, thesis, Universiti Teknologi MARA (UiTM).
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
description The objective of this project is to do preliminary design of 19 passengers multipurpose airplane. The airplane configuration consists of high wing, two turboprop engines, conventional tail and non-retractable tricycle landing gear. The airplane is designed according FAR 23 regulation. The aircraft operates at the rural to urban area. The analysis involves parametric sizing, undercarriage layout, weight and balance, stability in static longitudinal and flight performance. It is shown that the airplane is stable (static longitudinal) by having negative C ma. In the end, the design requirement and actual perform will be compared.
format Thesis
author Abdul Rauf, Mohd Taha
spellingShingle Abdul Rauf, Mohd Taha
Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
author_facet Abdul Rauf, Mohd Taha
author_sort Abdul Rauf, Mohd Taha
title Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
title_short Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
title_full Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
title_fullStr Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
title_full_unstemmed Preliminary design of 19 passengers multipurpose airplane / Mohd Taha Abdul Rauf
title_sort preliminary design of 19 passengers multipurpose airplane / mohd taha abdul rauf
publishDate 2002
url https://ir.uitm.edu.my/id/eprint/73890/1/73890.pdf
https://ir.uitm.edu.my/id/eprint/73890/
_version_ 1800100670555029504
score 13.18916

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