Investigation of the possibility of boundary layer control at the parts of aircraft (Q2755190)
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scientific article; zbMATH DE number 1669699
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Investigation of the possibility of boundary layer control at the parts of aircraft |
scientific article; zbMATH DE number 1669699 |
Statements
8 November 2001
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boundary layer control
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aircraft
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separation flow
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thermocouple thermoanemometer
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0.8440145
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0.84214264
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0.83950984
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0.83854455
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0.83647126
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0.83367115
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Investigation of the possibility of boundary layer control at the parts of aircraft (English)
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The results of experiment-based research for airfoils with separation flow control are presented. Analysis is carried out on the basis of signals of a thermocouple thermoanemometer for low velocities of gas and fluid flows. The work offers the experimentally proven possibility to more effective control the wing mechanization based on the detailed data on boundary layer obtained from the system of thermocouple thermoanemometer sensors.
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