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Contour of complete nonuniqueness as a method of structural optimization with stability constraints

✍ Scribed by M. Markiewicz; M. Życzkowski

Book ID
105010673
Publisher
Springer
Year
1981
Tongue
English
Weight
384 KB
Volume
35
Category
Article
ISSN
0022-3239

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An optimization procedure is developed to address the problem of seroelastic stability of high speed prop-rotor aircraft. A composite box beam is used as a perturbational stiffness model and the objective function to be minimized is the perturbational weight. An optimization algorithm, which used th