Modeling of the boundary conditions when calculating the stress-strain state of a cone-shaped aircraft nose fairing

Modeling of the boundary conditions when calculating the stress-strain state of a cone-shaped aircraft nose fairing

The stress-strain state of a cone-shaped aircraft nose fairing is studied. The structure is loaded with external pressure at high temperatures. The cone-shaped fairing has a weakened section with a modified value of the elastic modulus. The boundary value problems are solved with a controlled error....

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Hauptverfasser: Vinogradov, Yu. I., Menkov, G. B.
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Menkov, G. B.
description The stress-strain state of a cone-shaped aircraft nose fairing is studied. The structure is loaded with external pressure at high temperatures. The cone-shaped fairing has a weakened section with a modified value of the elastic modulus. The boundary value problems are solved with a controlled error. Based on the calculation results, it is concluded to simulate the boundary conditions in the form of a conjugation of a cone-shaped fairing with a cylindrical body.
doi_str_mv 10.1063/1.5133323
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title Modeling of the boundary conditions when calculating the stress-strain state of a cone-shaped aircraft nose fairing
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