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Development of a floating element photoelastic force balance

Development of a floating element photoelastic force balance
Development of a floating element photoelastic force balance
We present a floating element force balance design that uses an optical measurement of the force using photoelastic stress analysis. The force sensing element consists of pins embedded in photoelastic polyurethane pads, which generate an internal stress when the floating element is loaded that is observed via a transmission polariscope. A series of known loads and their corresponding fringe patterns allow a calibration matrix to be derived using a polynomial model solved by least squares regression. Finite Element Analysis (FEA) simulation is carried out to validate the proposed method. The balance then measured a lift curve of the NACA0015 wing at low speed. A comparison of the photoelastic balance and a commercial, 6-axis strain-gauge load cell showed typical differences of less than 6%. This optical approach enables accurate measurements with inexpensive and simple components inside the sensor. This work demonstrates that a photoelastic balance is a simple, inexpensive, and sensitive force transducer.
0723-4864
McLaughlin, Bradley
fd052519-4aaf-45b5-bcd1-79a1812f34c1
Lawson, John
4e0b1895-51c5-41e6-9322-7f79e76e0e4c
Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052
McLaughlin, Bradley
fd052519-4aaf-45b5-bcd1-79a1812f34c1
Lawson, John
4e0b1895-51c5-41e6-9322-7f79e76e0e4c
Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052

McLaughlin, Bradley, Lawson, John and Ganapathisubramani, Bharathram (2023) Development of a floating element photoelastic force balance. Experiments in Fluids, 64 (7), [126]. (doi:10.1007/s00348-023-03664-1).

Record type: Article

Abstract

We present a floating element force balance design that uses an optical measurement of the force using photoelastic stress analysis. The force sensing element consists of pins embedded in photoelastic polyurethane pads, which generate an internal stress when the floating element is loaded that is observed via a transmission polariscope. A series of known loads and their corresponding fringe patterns allow a calibration matrix to be derived using a polynomial model solved by least squares regression. Finite Element Analysis (FEA) simulation is carried out to validate the proposed method. The balance then measured a lift curve of the NACA0015 wing at low speed. A comparison of the photoelastic balance and a commercial, 6-axis strain-gauge load cell showed typical differences of less than 6%. This optical approach enables accurate measurements with inexpensive and simple components inside the sensor. This work demonstrates that a photoelastic balance is a simple, inexpensive, and sensitive force transducer.

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Accepted/In Press date: 6 June 2023
Published date: 1 July 2023
Additional Information: Funding Information: The authors are grateful for financial support from the Engineering and Physical Sciences Research Council (Ref No: EP/S013296/1 and EP/W026090/1). Publisher Copyright: © 2023, The Author(s).

Identifiers

Local EPrints ID: 481091
URI: http://eprints.soton.ac.uk/id/eprint/481091
ISSN: 0723-4864
PURE UUID: e2bde7af-4277-4c3b-9ec4-cf893e35b5f8
ORCID for John Lawson: ORCID iD orcid.org/0000-0003-3260-3538
ORCID for Bharathram Ganapathisubramani: ORCID iD orcid.org/0000-0001-9817-0486

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Date deposited: 15 Aug 2023 16:47
Last modified: 17 Mar 2024 03:53

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Contributors

Author: Bradley McLaughlin
Author: John Lawson ORCID iD

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