19th AIAA Applied Aerodynamics Conference 2001
DOI: 10.2514/6.2001-1327
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Reliability, weight, and cost tradeoffs in the design of composite laminates for cryogenic environments

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Cited by 12 publications
(12 citation statements)
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“…Qu et al [27] did a study of reliability, weight, and cost tradeoffs in composite laminates for cryogenic applications in which the composites would be subject to significant mechanical loading. Their paper indicated that to reduce the residual stresses that cause micro-cracking, laminates with small changes in angle between plies could be used.…”
Section: Micro-cracks / CMmentioning
confidence: 99%
“…Qu et al [27] did a study of reliability, weight, and cost tradeoffs in composite laminates for cryogenic applications in which the composites would be subject to significant mechanical loading. Their paper indicated that to reduce the residual stresses that cause micro-cracking, laminates with small changes in angle between plies could be used.…”
Section: Micro-cracks / CMmentioning
confidence: 99%
“…Qu et al (2003) investigated different response surface options for performing reliability-based optimization of composite laminates. Two sets of response surface approximations were used.…”
Section: Approximations In Reliability-based Designmentioning
confidence: 99%
“…Response surface approximation can filter the noise in the response functions obtained from either physical experiments or numerical solutions. Since the approximation is a simple polynomial function, it is inexpensive to use for procedures such as global optimization (Liu et al 2000), discrete variable optimization (Harrison et al 1995), and non-deterministic design (Qu et al 2003) which require a large number of function evaluations. Since each response surface can be generated independently, it is possible for experts to develop their own models and combine them for multidisciplinary design optimization.…”
Section: Approximations In Reliability-based Designmentioning
confidence: 99%
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