Solution of the problem of optimum boundary layer control on the porous surface of a turbine blade (Q1339612)
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scientific article; zbMATH DE number 699585
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Solution of the problem of optimum boundary layer control on the porous surface of a turbine blade |
scientific article; zbMATH DE number 699585 |
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Solution of the problem of optimum boundary layer control on the porous surface of a turbine blade (English)
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6 December 1994
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Problems of the optimization of coolant injection into a laminar compressible gas boundary layer are considered within the framework of the integral method of boundary layer calculation. The blade surface temperature is not given, but is found in the process of solving the problem, appearing as a control. The variational problems are solved using the Pontryagin maximum principle.
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coolant injection
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integral method
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Pontryagin maximum principle
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0.8830261
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0.83947605
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0.8390928
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0.8382975
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0.83730567
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0.8343144
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