42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2006

DOI: 10.2514/6.2006-5123

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Effects of Production Variations on the Reliability of a Solid Rocket Motor

Kenan Bozkaya¹,

Bayindir Kuran²,

Mehmet Sinan Hasanoglu³

et al.

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Cited by 4 publications

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“…The reliability of the composite configuration was also calculated. Bozkaya et al [18,19] and Akpan and Wong [20] developed some useful and efficient methods for the sensitivity analysis and reliability calculations [21] based on surface response methods (SRM) and Monte Carlo simulation techniques.…”

Section: Introductionmentioning

confidence: 99%

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Xie¹,

Yang²,

et al. 2019

Journal of Spacecraft and Rockets

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We describe in this paper a methodology to perform the probabilistic and reliabilitybased design of a novel carbon/carbon rocket nozzle subjected to operational thermal and mechanical loads. In this methodology the nozzle is represented by a multiphysics finite element model capable of predicting the temperature and stress fields of the exit cone. The analysis shows

“…The reliability of the composite configuration was also calculated. Bozkaya et al [18,19] and Akpan and Wong [20] developed some useful and efficient methods for the sensitivity analysis and reliability calculations [21] based on surface response methods (SRM) and Monte Carlo simulation techniques.…”

Section: Introductionmentioning

confidence: 99%

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Xie¹,

Yang²,

et al. 2019

Journal of Spacecraft and Rockets

View full text Add to dashboard Cite

We describe in this paper a methodology to perform the probabilistic and reliabilitybased design of a novel carbon/carbon rocket nozzle subjected to operational thermal and mechanical loads. In this methodology the nozzle is represented by a multiphysics finite element model capable of predicting the temperature and stress fields of the exit cone. The analysis shows

Robust Regression Metamodelling of Complex Systems: The Case of Solid Rocket Motor Performance Metamodelling

¹

,

²

,

³

2012

Advances in Intelligent Modelling and Simulation

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Robust Design Optimization for Multiple Responses Using Response Surface Methodology and Taguchi Approach: Solid Rocket Motor Application

¹

,

²

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³

2007

48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

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No abstract

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