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Monte Carlo Simulation Methodology For The Reliability Of Aircraft Structures - Andreas Rambalakos
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ISBN: 9783836473484

ID: 9783836473484

Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level. Textbooks New, Books~~Technology~~Engineering (General), Monte-Carlo-Simulation-Methodology-For-The-Reliability-Of-Aircraft-Structures~~Andreas-Rambalakos, 999999999, Monte Carlo Simulation Methodology For The Reliability Of Aircraft Structures, Andreas Rambalakos, 3836473488, VDM Verlag Dr. Mueller e.K., , , , , VDM Verlag Dr. Mueller e.K.

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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures - Reliability of Aircraft Structures Under Damage Tolerance Requirements
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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures - Reliability of Aircraft Structures Under Damage Tolerance Requirements - Taschenbuch

2008, ISBN: 9783836473484

[ED: Taschenbuch / Paperback], [PU: VDM Verlag Dr. Müller], Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level., Neuware, gewerbliches Angebot, 220 mm, [GW: 235g]

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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures - Rambalakos, Andreas
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Rambalakos, Andreas:
Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures - Taschenbuch

2008

ISBN: 9783836473484

[ED: Softcover], [PU: Vdm Verlag Dr. Müller], Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level.2008. 172 S. 220 mmVersandfertig in 3-5 Tagen, [SC: 0.00]

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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures - Andreas Rambalakos
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Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level. Bücher / Naturwissenschaften, Medizin, Informatik & Technik / Naturwissenschaften allgemein

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Monte Carlo Simulation Methodology for the Reliability of Aircraft ... - Andreas Rambalakos
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Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level. Buch / Broschur

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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures
Autor:

Rambalakos, Andreas

Titel:

Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures

ISBN-Nummer:

9783836473484

Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the system capacity cumulative distribution function are expanded from three elements in the current literature up to six elements. The second objective is to compute the probability of failure of a fuselage skin lap joint under static load conditions by examining the residual strength of the fasteners when subjected to various load distributions initially and following subsequent fastener sequential failures. The last objective is to present a MCS methodology for computing the non-periodic inspections required in order to maintain a prescribed minimum reliability level.

Detailangaben zum Buch - Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures


EAN (ISBN-13): 9783836473484
ISBN (ISBN-10): 3836473488
Taschenbuch
Erscheinungsjahr: 2008
Herausgeber: VDM Verlag
168 Seiten
Gewicht: 0,267 kg
Sprache: ger/Deutsch

Buch in der Datenbank seit 29.05.2008 15:21:20
Buch zuletzt gefunden am 25.10.2016 11:31:25
ISBN/EAN: 9783836473484

ISBN - alternative Schreibweisen:
3-8364-7348-8, 978-3-8364-7348-4

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