A refined optimality criterion technique applied to aircraft wing structural design (Q3476414)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | A refined optimality criterion technique applied to aircraft wing structural design |
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A refined optimality criterion technique applied to aircraft wing structural design (English)
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1989
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optimal design
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finite element method
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refined optimality criterion method
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sensitivity analysis
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FORTRAN-77
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modular computer program `ARS 4'
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Automatic Resizing System 4
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wing structures subjected to size, stress, displacement, and buckling constraints
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Kuhn-Tucker conditions
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fully stressed design
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