On the Performance of Small-Sized Venturi Flowmeters in Cavitating and Non-Cavitating Flow Regimes

被引:0
|
作者
Kandula, Max [1 ]
Nufer, Brian M. [2 ]
机构
[1] NASA, KBR, Mail Stop LASSO 001, Kennedy Space Ctr, FL 32899 USA
[2] NASA, Explorat Payloads Branch, Kennedy Space Ctr, FL 32899 USA
来源
AIAA SCITECH 2024 FORUM | 2024年
关键词
ORIFICE PLATE;
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The performance of venturi in the cavitating and non-cavitating flow regimes has been discussed theoretically and experimentally. Pressure drop test data with water was obtained with a 0.0355 inch throat venturi with pressure drop measured between the inlet and the outlet of the venturi, typical of practical venturi measurements on spacecraft. The pressure drop data acquired in the non-cavitating regime at relatively low flow rates display low Reynolds number effects on the discharge coefficient. A theoretical discussion of the corresponding discharge coefficients in the two flow regimes along with comparisons with test data are presented. For non-cavitating flow regime of unique venturi geometries of relatively small throat size, test data required low Reynolds number correction factor for the discharge coefficient in terms of throat Reynolds number. The application of existing theory is not straightforward for the unique geometries under consideration.
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页数:12
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