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Design and Analysis of Integrally  and Riveted Stiffened Panel - Muhammad Adeel
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Muhammad Adeel:

Design and Analysis of Integrally and Riveted Stiffened Panel - Taschenbuch

ISBN: 9783845422909

ID: 9783845422909

A Numerical Technique for Analyzing Metallic Stiffened Panel In this research first the analysis of integrally stiffened panel has been made using FE code ANSYS. Hoop, Axial and Radial stress are calculated for the stiffened panel subjected to internal pressure. Secondly, crack growth characteristics of the integrally stiffened panel and conventional stiffened panel based on fracture mechanics and FE analysis are investigated. A fourteen-stringer stiffened panel is analyzed for a central skin crack propagating towards the adjacent stringers. Stress intensity factors and fatigue crack propagation rates of both types of the stiffened panels are then compared. The analyses result show that integral stiffening cause higher stress intensity factor than conventional stiffened panel as the crack tip passes through the stringer and the integral stiffened panel has less damage tolerance capability than the riveted stiffened panel. Finally, the FE analysis of repaired integrally stiffened aluminum alloy panel with a circumferential crack has performed in ANSYS. The analysis results depict that the maximum von Mises stress in each component of the repaired panel is below the yield strength of the Al alloy so the repaired method is successful. Design and Analysis of Integrally and Riveted Stiffened Panel: In this research first the analysis of integrally stiffened panel has been made using FE code ANSYS. Hoop, Axial and Radial stress are calculated for the stiffened panel subjected to internal pressure. Secondly, crack growth characteristics of the integrally stiffened panel and conventional stiffened panel based on fracture mechanics and FE analysis are investigated. A fourteen-stringer stiffened panel is analyzed for a central skin crack propagating towards the adjacent stringers. Stress intensity factors and fatigue crack propagation rates of both types of the stiffened panels are then compared. The analyses result show that integral stiffening cause higher stress intensity factor than conventional stiffened panel as the crack tip passes through the stringer and the integral stiffened panel has less damage tolerance capability than the riveted stiffened panel. Finally, the FE analysis of repaired integrally stiffened aluminum alloy panel with a circumferential crack has performed in ANSYS. The analysis results depict that the maximum von Mises stress in each component of the repaired panel is below the yield strength of the Al alloy so the repaired method is successful., LAP Lambert Acad. Publ.

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Design and Analysis of Integrally and Riveted Stiffened Panel - Muhammad Adeel
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Muhammad Adeel:

Design and Analysis of Integrally and Riveted Stiffened Panel - neues Buch

ISBN: 9783845422909

ID: a3f0cff60979da1640c7b725d87e9b8a

In this research first the analysis of integrally stiffened panel has been made using FE code ANSYS. Hoop, Axial and Radial stress are calculated for the stiffened panel subjected to internal pressure. Secondly, crack growth characteristics of the integrally stiffened panel and conventional stiffened panel based on fracture mechanics and FE analysis are investigated. A fourteen-stringer stiffened panel is analyzed for a central skin crack propagating towards the adjacent stringers. Stress intensity factors and fatigue crack propagation rates of both types of the stiffened panels are then compared. The analyses result show that integral stiffening cause higher stress intensity factor than conventional stiffened panel as the crack tip passes through the stringer and the integral stiffened panel has less damage tolerance capability than the riveted stiffened panel. Finally, the FE analysis of repaired integrally stiffened aluminum alloy panel with a circumferential crack has performed in ANSYS. The analysis results depict that the maximum von Mises stress in each component of the repaired panel is below the yield strength of the Al alloy so the repaired method is successful. Bücher / Naturwissenschaften, Medizin, Informatik & Technik / Technik / Maschinenbau

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Design And Analysis Of Integrally And Riveted Stiffened Panel - Muhammad Adeel
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(*)
Muhammad Adeel:
Design And Analysis Of Integrally And Riveted Stiffened Panel - Taschenbuch

ISBN: 9783845422909

ID: 9783845422909

Design And Analysis Of Integrally And Riveted Stiffened Panel Design-and-Analysis-of-Integrally-and-Riveted-Stiffened-Panel~~Muhammad-Adeel Science/Tech>Engineering>Engr Ref Paperback, AV Akademikerverlag GmbH & Co. KG.

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Design and Analysis of Integrally and Riveted Stiffened Panel A Numerical Technique for Analyzing Metallic Stiffened Panel - Muhammad Adeel
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Muhammad Adeel:
Design and Analysis of Integrally and Riveted Stiffened Panel A Numerical Technique for Analyzing Metallic Stiffened Panel - neues Buch

ISBN: 9783845422909

ID: 9783845422909

Design and Analysis of Integrally and Riveted Stiffened Panel A Numerical Technique for Analyzing Metallic Stiffened Panel Author :Muhammad Adeel 9783845422909 3845422904

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Design and Analysis of Integrally and Riveted Stiffened Panel - Adeel, Muhammad
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Adeel, Muhammad:
Design and Analysis of Integrally and Riveted Stiffened Panel - Taschenbuch

2011, ISBN: 3845422904

ID: 13788745242

[EAN: 9783845422909], Neubuch, [PU: LAP Lambert Academic Publishing], This item is printed on demand for shipment within 3 working days.

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Design and Analysis of Integrally  and Riveted Stiffened Panel
Autor:

Adeel, Muhammad

Titel:

Design and Analysis of Integrally and Riveted Stiffened Panel

ISBN-Nummer:

9783845422909

Detailangaben zum Buch - Design and Analysis of Integrally and Riveted Stiffened Panel


EAN (ISBN-13): 9783845422909
ISBN (ISBN-10): 3845422904
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2011
Herausgeber: AV Akademikerverlag GmbH & Co. KG.

Buch in der Datenbank seit 10.01.2009 07:40:09
Buch zuletzt gefunden am 26.09.2016 12:16:06
ISBN/EAN: 9783845422909

ISBN - alternative Schreibweisen:
3-8454-2290-4, 978-3-8454-2290-9

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