Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft (Q3316712)
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scientific article
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft |
scientific article |
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Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft (English)
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1984
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all variables have to be considered
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aeroelastic tailoring
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multivariable optimization problem
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transformation
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aeroelastic equations of motion
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composite swept wing
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critical aeroelastic characteristics for flutter and divergence
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expressible in terms of three bounded generic stiffness variables and the fiber orientation angle
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