Development of a numerical model designed to calculate the temperature field and thermal stresses in structural elements of aircrafts (Q2686693)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Development of a numerical model designed to calculate the temperature field and thermal stresses in structural elements of aircrafts |
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Development of a numerical model designed to calculate the temperature field and thermal stresses in structural elements of aircrafts (English)
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28 February 2023
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quasistatic thermoelasticity problem
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gas dynamics
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boundary layer
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effective length
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two-step finite difference scheme
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