An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro

Damages in aircraft structures are classified as negligible or intolerable. Intolerable damage should be repaired to maintain airworthiness of the aircraft. One of the damages covered in this paper is crack damage and the repair on it. The damage location in this paper is on the skin next to the str...

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Format: Article
Language:English
Published: Faculty of Mechanical Engineering and University Publication Centre (UPENA) 2007
Online Access:http://ir.uitm.edu.my/id/eprint/17537/
http://ir.uitm.edu.my/id/eprint/17537/1/AJ_RAMZYZAN%20RAMLY%20JME%2007.pdf
id uitm-17537
recordtype eprints
spelling uitm-175372017-08-01T06:45:33Z http://ir.uitm.edu.my/id/eprint/17537/ An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro Damages in aircraft structures are classified as negligible or intolerable. Intolerable damage should be repaired to maintain airworthiness of the aircraft. One of the damages covered in this paper is crack damage and the repair on it. The damage location in this paper is on the skin next to the stringer section. Most damage repair methods and procedures are prescribed in the Structural Repair Manual (SRM). This paper presents strength/stress analysis on the section (stiffened panel) before damage, after damage, and after repair using bonded patch. Finite Element Analysis (FEA) software called ANSYS was used. An experimental method was used to validate the FEA method. The results of the analysis showed that the strength of the repaired structure was restored. Both methods showed agreement in the results pattern. Faculty of Mechanical Engineering and University Publication Centre (UPENA) 2007 Article PeerReviewed text en http://ir.uitm.edu.my/id/eprint/17537/1/AJ_RAMZYZAN%20RAMLY%20JME%2007.pdf UNSPECIFIED (2007) An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro. Journal of Mechanical Engineering, 14 (1). pp. 45-59. ISSN 1823-5514
repository_type Digital Repository
institution_category Local University
institution Universiti Teknologi MARA
building UiTM Institutional Repository
collection Online Access
language English
description Damages in aircraft structures are classified as negligible or intolerable. Intolerable damage should be repaired to maintain airworthiness of the aircraft. One of the damages covered in this paper is crack damage and the repair on it. The damage location in this paper is on the skin next to the stringer section. Most damage repair methods and procedures are prescribed in the Structural Repair Manual (SRM). This paper presents strength/stress analysis on the section (stiffened panel) before damage, after damage, and after repair using bonded patch. Finite Element Analysis (FEA) software called ANSYS was used. An experimental method was used to validate the FEA method. The results of the analysis showed that the strength of the repaired structure was restored. Both methods showed agreement in the results pattern.
format Article
title An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
spellingShingle An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
title_short An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
title_full An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
title_fullStr An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
title_full_unstemmed An analysis of stress over a bonded repaired stiffened panel / Ramzyzan Ramly and Wahyu Kuntjoro
title_sort analysis of stress over a bonded repaired stiffened panel / ramzyzan ramly and wahyu kuntjoro
publisher Faculty of Mechanical Engineering and University Publication Centre (UPENA)
publishDate 2007
url http://ir.uitm.edu.my/id/eprint/17537/
http://ir.uitm.edu.my/id/eprint/17537/1/AJ_RAMZYZAN%20RAMLY%20JME%2007.pdf
first_indexed 2023-09-18T22:58:32Z
last_indexed 2023-09-18T22:58:32Z
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