Abstract
A method is described for compensating the errors of measurement of flow parameters in wind tunnels and determination of the high-speed flight parameters of aircraft. The method is based on design modifications of the measurement system sensing devices with a view toward affecting the local characteristics of flow past the total- or static-pressure intakes.
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References
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Additional information
Translated from Izmeritel'naya Tekhnika, No. 2, pp. 33–35, February, 1996.
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Petunin, A.N. Aerodynamic compensation in pressure sensors used for the measurement of flow parameters. Meas Tech 39, 168–172 (1996). https://doi.org/10.1007/BF02378944
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DOI: https://doi.org/10.1007/BF02378944