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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures

9783836473484 | Rambalakos, Andreas
Rambalakos, Andreas, Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures, 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.
 
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Detailangaben zum Buch - Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures

Neupreis: 68,00 EUR
EAN (bzw. ISBN-13): 9783836473484
ISBN (ISBN-10): 3836473488
Taschenbuch
Erscheinungsjahr: 2008
Herausgeber: VDM Verlag
168 Seiten
Gewicht: 0,267 kg
Sprache: ger/Deutsch

In der Datenbank seit 29.05.2008 15:21:20
Zuletzt gefunden am 22.10.2011 22:53:15
ISBN/EAN: 9783836473484

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Weitere Angaben zum Buch
ISBN - alternative Schreibweisen: 978-3-836-47348-4, 978-3-8364-7348-4, 978-3-83647-348-4, 978-3-836473-48-4, 978-3-8364734-8-4
EAN (bzw. neue ISBN) - alternative Schreibweisen: 978-3-836-47348-4, 978-3-8364-4734-4, 978-3-83647-473-4, 978-3-836473-47-4, 978-3-8364734-4-4
Alternative Schreibweisen:
Titel: Monte Carlo Simulation, Aircraft The Raf, Damage Tolerance, Structures

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

ISBN: 9783836473484, Preisentwicklung...

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., [PU: VDM Verlag Dr. Müller], [CT: Varia]

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Andreas Rambalakos:
Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures (Reliability of Aircraft Structures Under Damage Tolerance Requirements)

ISBN: 3836473488, Preisentwicklung...

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., EAN: 9783836473484, ISBN: 3836473488 [SW:Monte-Carlo-Methode ; Luftwaffe], [VÖ:20080400], Buch (dtsch.)

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Andreas Rambalakos:
Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures (Reliability of Aircraft Structures Under Damage Tolerance Requirements)

ISBN: 3836473488, Preisentwicklung...

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., EAN: 9783836473484, ISBN: 3836473488 [SW:Monte-Carlo-Methode ; Luftwaffe], [VÖ:20080400], Buch (dtsch.)

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