Preview

Izmeritel`naya Tekhnika

Advanced search
Open Access Open Access  Restricted Access Subscription Access

Static component of the temperature error of the strain-gauge balance: determination of the temperature sensitivity coeficient

https://doi.org/10.32446/0368-1025it.2021-10-8-13

Abstract

High precision strain gauge balances are used for the testing of the arcraft models in wind tunnels. The precision of the strain gauge balances depends on the balance temperature. The basic physical factors affecting the balance readings with temperature variation are reviewed and estimated. We considered the effect of static component of the temperature error on the readings of the strain gauge balance. A method of application of temperature corrections to the balance readings by means of the temperature sensitivity coefficient is described. We developed the method of determining coefficient of temperature sensitivity of balance components during a fulfilment of the test campaign in a wind tunnel. The experimental equipment and the experimental investigations carried out are described. The experimental results of determining the effect of the static temperature component on the readings of six-component balance are presented. Characteristic value of the sensitivity coefficient was found to be approximately 0.04 %/°C. It is shown that the standard deviation of the balance readings exceeds the balance calibration standard deviation when the balance temperature varies more than 3–4 °C. The temperature systematic error has to be excluded from results of the balance measurement in the form of correction to the sensitivity coefficient or electrical signal. The method was verified by the results of measurement of the weight of the aircraft model and the weight of the metric parts of the strain-gauge balance’s longitudinal and normal force components in the wind tunnel.

 

About the Authors

A. R. Gorbushin
Moscow Institute of Physics and Technology (National Research University); Central Aerohydrodynamic Institute
Russian Federation

Anton R. Gorbushin

Dolgoprudny, Moscow region

Zhukovsky, Moscow region



E. A. Krapivina
Central Aerohydrodynamic Institute
Russian Federation

Ekaterina A. Krapivina

Zhukovsky, Moscow region



M. N. Tytyk
Central Aerohydrodynamic Institute
Russian Federation

Marina N. Tytyk

Zhukovsky, Moscow region



References

1. Ewald B. F. R., Measurement Science and Technology, 2000, vol. 11, no. 6, рр. 81–94. https://doi.org/10.1088/0957-0233/11/6/201

2. Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing, AIAA Rec. Practice, 2020 AIAA R-091A-2020. https://doi.org/10.2514/4.106019.001

3. Bogdanov V. V., Volobuev V. S., A multi-component straingage balance, Sensors and Systems, 2004, no. 3, pp. 3–9. (In Russ.)

4. Volobuev V. S., Gorbushin A. R., Pervye aehrodinamicheskie vesy Rossii, Trudy TsAGI, 2015, iss. 2744, pp. 1–30. (In Russ.)

5. Rhew R., Parker P., 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conferenc, 5–9 June 2017, Denver, Colorado, AIAA 2017-4427. https://doi.org/10.2514/6.2017-4427

6. Burov V. V., Volobuev V. S., Glazkov S. A., Gorbushin A. R., Chumachenko E. K., Automation and Remote Control, 2011, vol. 72, pp. 634–641. https://doi.org/10.1134/S0005117911030143

7. Rivers M. B., Rudnik R., Quest J., 53rd AIAA Aerospace Sciences Meeting, AIAA SciTech, 5–9 January 2015, Kissimmee, Florida , AIAA 2015-1093. https://doi.org/10.2514/6.2015-1093

8. Wood M. N., Capps D. S., The accurate measurements of drag in the 8 FT×8 FT tunnel, Aerodynamic data accuracy and quality: requirements and capabilities in wind tunnel testing, AGARD Conferences Proceeding 429, 1985, р. 9.

9. Frank L., Experience relative to the interaction between balance engineer and the project engineer with regard to measurement uncertainty, Proceedings of a symposium sponsored by the National Aeronautics and Space Administration, Washington, D.C., Langley Research Center, Hampton, Virginia, USA, October 22– 25, 1996, NASA/CP-1999-209101/PT1, pp. 243–277.

10. Bukharov K. D., Gorbushin A. R., Kartashev Yu. V., Petronevich V. V., Sudakova I. A., Chernyshev S. L., TsAGI Science Journal, 2017, vo l. 48, iss.7, pp. 627–647. http s://doi.org/10.1615/TsAGISciJ.2018026242

11. Klokova N. P., Tenzorezistory: Teoriya, metodika rascheta, razrabotki, Moscow, Mashinostroenie Publ., 1990. (In Russ.)

12. Bogdanov V. V., Gorbushin A. R., Volobuyev V. S., TsAGI Science Journal, 2009, vol. 40, iss. 5, pp. 619–629. https://doi.org/10.1615/TsAGISciJ.v40.i5.80

13. Volobuyev V. S., Gorbushin A. R., Sudakova I. A., Tikhomirov V. I., TsAGI Science Journal, 2017, vol. 48, iss. 2, pp. 187–197. https://doi.org/10.1615/TsAGISciJ.2017021104

14. Quest J., Schimanski D., 41st Aerospace Sciences Meeting and Exhibit, 06–09 January 2003, Reno, Nevada, AIAA 2003-755. https://doi.org/10.2514/6.2003-755

15. Simpson J., Landman D., Giroux R., Zeisset M., Hall B., Rhew R., 2005 U.S. Air Force T&E Days, 06–08 December 2005, Nashville, Tennessee, AIAA 2005-7601. https://doi.org/10.2514/6.2005-7601

16. Toro K., Burns D., Parker P. A., 2018 Aerodynamic Measurement Technology and Ground Testing Conference, June 25–29, 2018, Atlanta, Georgia, AIAA 2018-4108. https://doi.org/10.2514/6.2018-4108

17. Landman D., Toro K. G., Commo S. A., Lynn K. C., Journal of Aircraft, 2015, vol. 52, no. 3. https://doi.org/10.2514/1.C032930

18. Gorbushin A. R., TsAGI Science Journal, 2009, vol. 40, iss. 4, pp. 485–495. https://doi.org/10.1615/TsAGISciJ.v40.i4.70

19. Tumanov A. T., Aviatsionnye materialy, Handbook in 9 volums, vol. 1 Konstruktsionnye stali, Moscow, VIAM, ONTI Publ., 1975. (In Russ.)


Review

For citations:


Gorbushin A.R., Krapivina E.A., Tytyk M.N. Static component of the temperature error of the strain-gauge balance: determination of the temperature sensitivity coeficient. Izmeritel`naya Tekhnika. 2021;(10):8-13. (In Russ.) https://doi.org/10.32446/0368-1025it.2021-10-8-13

Views: 121


ISSN 0368-1025 (Print)
ISSN 2949-5237 (Online)