Performance optimization of multidisciplinary mechanical systems subject to uncertainties

Oakley, David R.; Sues, Robert H.; Rhodes, Graham S.

doi:10.1016/s0266-8920(97)00004-0

Cited by 41 publications

(19 citation statements)

References 4 publications

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“…Another efficient single-loop approach based on adaptive response surfaces was developed by Sues et al [22][23][24] and is described in Section 34.5. All of these methods simplify the reliability calculations.…”

Section: Review Of Rbdo Methodsmentioning

confidence: 99%

Applications of Reliability Assessment

Sues¹,

Shin²,

Wu³

2004

Engineering Design Reliability Handbook

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This example considers a detailed airplane wing design problem [38]. The baseline airplane is a Mach 0.3, 20-seat transport with a payload capacity on the order of 5000 lb. RBDO FormulationObjective: Maximize expected cruise range Subject to reliability constraints: P(upper surface root stress 1 £ yield) ≥ 99.0% P(upper surface root stress 2 £ yield) ≥ 99.0% P(lower surface root stress 1 £ yield) ≥ 99.0% P(lower surface root stress 2 £ yield) ≥ 99.0% P(takeoff distance £ 3000 ft) ≥ 99.0% P(wing area £ 600 ft 2 ) ≥ 50.0%

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Section: Review Of Rbdo Methodsmentioning

confidence: 99%

Applications of Reliability Assessment

Sues¹,

Shin²,

Wu³

2004

Engineering Design Reliability Handbook

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show abstract

“…In the last decade the topic has gained larger attention also for its suitability to robust design and design under uncertainties, [PSP93,OSR98,DC00]. As a matter of fact many computer codes are available which deal with reliability analysis and related topics (Isight, Nessus, Dakota, MSC.Robust Design, etc.).…”

Section: State Of the Artmentioning

confidence: 99%

Reliability based analysis of the crosswind stability of railway vehicles

Carrarini

2007

Journal of Wind Engineering and Industrial Aerodynamics

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“…A generic framework for the stochastic multidisciplinary design has been proposed by Du and Chen [109] and Oakley [110]. For aircraft design, multidisciplinary approaches have been presented by Mavris and coworkers [111][112][113], accounting for various sources of uncertainties, such as modeling and economic variability, and aiming for system affordability.…”

Section: Rbdo Of Aircraft Systemsmentioning

confidence: 99%