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On the Performance of Small-Sized Venturi Flowmeters in Cavitating and Non-Cavitating Flow RegimesThe 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.
Document ID
20220016071
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Max Kandula
(Stinger Ghaffarian Technologies (United States) Greenbelt, Maryland, United States)
Brian M Nufer
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
October 25, 2022
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA 2023 Aviation Forum
Location: San Diego, CA
Country: US
Start Date: June 12, 2023
End Date: June 16, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 000278
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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