Pomiar przepływu ciepła przy wykorzystaniu farby termoczułej
Heat transfer measurements using thermal sensitive paint
Keywords:
farba termoczuła, pomiar temperatury, metoda TSP
Abstract
W artykule omówiony został problem pomiaru powierzchniowego rozkładu temperatury przy pomocy farby termoczułej. Przedstawiono proces pomiarowy, począwszy od kalibracji farby a skończywszy na pomiarach chłodzenia przy użyciu tej techniki.
References
1. Nowak J., Bezpieczeństwo samochodów i ruchu drogowego, WKiŁ, Warszawa 2004.
2. Liu, T. and Sullivan, J.P., 2005, Pressure and Temperature Sensitive Paints, Springer, New York.
3. Jahanmiri, M., 2011, “Pressure Sensitive Paints: The Basics & Applications,” 2011:07, Chalmers University of Technology, Göte-borg, Sweden.
4. Cottingham, T., 2015, “Characterization and Optimization of Temperature-Sensitive Microbeads for Simultaneous Thermome-try and Velocimetry for Fluid Dynamic Applications,” M.Sc. thesis, University of Washington.
5. Sullivan, J., 2009, “Molecular Sensors – Temperature Sensitive Paint”, https://slideplayer.com/slide/1675994/
6. Luminescent Paint,” Ph.D. thesis, Nanjing University of Aeronautics and Astronautics.
7. Rosłowicz, A. and Bednarczyk, P., 2017, “Analysis of Heat Trans-fer in a Supersonic Rocket Head,” Transactions of the Institute of Aviation, No. 1 (246), pp.79-94.
8. Fonov, S., Crafton, J., Goss, L., Jones, G., Fonov, S. and Tyler, C., 2005, “Multi-Aspect Solutions for Moving Vehicle Testing,” RTO-MP-AVT-124-5, NATO Science and Technology Organisation.
9. Stokes, N., Patel, S. and Hahn, M., 2012, “Boundary Layer Transition Detection Using Temperature Sensitive Paint in the ARA Transonic Wind Tunnel,” ICAS 2012-3.4.2, 28th International Congress of the Aeronautical Sciences, Brisbane, Australia.
10. Borovoy, V., Mosharov, V., Noev, A. and Radchenko, V., 2012, “Temperature Sensitive Paint Application for Investigation of Boundary Layer Transition in Short-Duration Wind Tunnels,” Progress in Flight Physics 3, pp. 15-24.
11. Crafton, J.W., 2004, “The Impingement of Sonic and Sub-Sonic Jets onto a Flat Plate at Inclined Angles,” Ph.D. Thesis, Purdue University.
12. Crafton, J., Ladchenko, N., Guille, M. and Sullivan, P., “Application of Temperature and Pressure Sensitive Paint to an Obliquely Im-pinging Jet,” 37th Aerospace Sciences Meeting and Exhibit, AIAA-99-0387, Reno, USA.
13. Liu, Q., 1993, “Study of Heat Transfer Characteristics if Impinging Air Jet Using Pressure and Temperature Sensitive Paint,” B.S. Nanjing University of Aeronautics and Astronautics.
14. Gao, L., 2003, “Effect of Jet Hole Arrays Arrangement on Impingement Heat Transfer,” M.Sc. thesis, Louisiana State University.
15. Zuniga, H. A., 2009, “Study of Film Cooling Effectiveness: Conical, Trenched and Asymmetrical Shaped Holes,” Ph.D. thesis, University of Central Florida, Orlando.
16. Wright, L. M., Gao, Z., Varvel, T. A., and Han, J.-C., “Assessment of Steady State PSP, TSP, and IR Measurement Techniques for Flat Plate Film Cooling,” Heat Transfer: Volume 3, ASME, 2005, pp. 37-46.
17. Kurits, I. and Norris, J. D., 2011, “Temperature-Sensitive Paint Calibration Methodology Developed at AEDC Tunnel 9,” AIAA 2011-851.
18. Schramm, J.M., Hannemann, K., Ozawa, H., Beck, W. and Klein, Ch., 2014, “Development of Temperature Sensitive Paints for the High Enthalpy Shock Tunnel Goettingen,” 8th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon.
19. Product catalog, 2017, Innovative Scientific Solutions Inc.
20. Jeziorek, Ł., 2017, “Rozwój Metodologii TSP (Farba Termoczuła) i Potencjału Badań Laboratoryjnych z Nią Związanych,” (ang. Development of Thermal Sensitive Paint Methodology and Its Research Capabilities), Sprawozdanie z pracy badawczej nr 2017/PS/01, Institute of Aviation, Warsaw.
21. Kercher, D.M., Tabakoff W., 1969, “Heat Transfer by a Square Array of Round Air Jets Impinging Perpendicular to a Flat Surface Including the Effect of Spent Air,” ASME paper 69-GT-4.
22. Floerschuetz, L.W., Metzger D.E., Truman C.R., 1981, “jet Array Impingement with Crossflow – correlation of streamwise Resolved Flow and Heat Transfer Distributions,” NASA Contractor Report 3373.
23. Chamberlain, J.E., 1966, “Heat Transfer Between a Turbulent Round Jet and a Segmented Plate Perpendicular to It,” M.Sc. thesis, Newark College of Engineering.
24. Szafran, K., Shcherbonos, O. and Ejmocki, D., 2014, “Effect of duct shape on ducted propeller trust performance,” Transactions of the Institute of Aviation, No. 4 (237), pp. 85-91.
25. Ruchała, P. and Szafran, K., 2016, ”Praktyczne Aspekty Zastoso-wania Otunelowanych Śmigieł Pchających,” (ang. The Aspects of Practical Application of Ducted Fans), Transactions of the Institute of Aviation, No. 3 (244), pp. 257-266.
26. Navarra, K. R., 1997, “Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications,” Ms.C. thesis, Virginia Polytechnic Institute and State University.
2. Liu, T. and Sullivan, J.P., 2005, Pressure and Temperature Sensitive Paints, Springer, New York.
3. Jahanmiri, M., 2011, “Pressure Sensitive Paints: The Basics & Applications,” 2011:07, Chalmers University of Technology, Göte-borg, Sweden.
4. Cottingham, T., 2015, “Characterization and Optimization of Temperature-Sensitive Microbeads for Simultaneous Thermome-try and Velocimetry for Fluid Dynamic Applications,” M.Sc. thesis, University of Washington.
5. Sullivan, J., 2009, “Molecular Sensors – Temperature Sensitive Paint”, https://slideplayer.com/slide/1675994/
6. Luminescent Paint,” Ph.D. thesis, Nanjing University of Aeronautics and Astronautics.
7. Rosłowicz, A. and Bednarczyk, P., 2017, “Analysis of Heat Trans-fer in a Supersonic Rocket Head,” Transactions of the Institute of Aviation, No. 1 (246), pp.79-94.
8. Fonov, S., Crafton, J., Goss, L., Jones, G., Fonov, S. and Tyler, C., 2005, “Multi-Aspect Solutions for Moving Vehicle Testing,” RTO-MP-AVT-124-5, NATO Science and Technology Organisation.
9. Stokes, N., Patel, S. and Hahn, M., 2012, “Boundary Layer Transition Detection Using Temperature Sensitive Paint in the ARA Transonic Wind Tunnel,” ICAS 2012-3.4.2, 28th International Congress of the Aeronautical Sciences, Brisbane, Australia.
10. Borovoy, V., Mosharov, V., Noev, A. and Radchenko, V., 2012, “Temperature Sensitive Paint Application for Investigation of Boundary Layer Transition in Short-Duration Wind Tunnels,” Progress in Flight Physics 3, pp. 15-24.
11. Crafton, J.W., 2004, “The Impingement of Sonic and Sub-Sonic Jets onto a Flat Plate at Inclined Angles,” Ph.D. Thesis, Purdue University.
12. Crafton, J., Ladchenko, N., Guille, M. and Sullivan, P., “Application of Temperature and Pressure Sensitive Paint to an Obliquely Im-pinging Jet,” 37th Aerospace Sciences Meeting and Exhibit, AIAA-99-0387, Reno, USA.
13. Liu, Q., 1993, “Study of Heat Transfer Characteristics if Impinging Air Jet Using Pressure and Temperature Sensitive Paint,” B.S. Nanjing University of Aeronautics and Astronautics.
14. Gao, L., 2003, “Effect of Jet Hole Arrays Arrangement on Impingement Heat Transfer,” M.Sc. thesis, Louisiana State University.
15. Zuniga, H. A., 2009, “Study of Film Cooling Effectiveness: Conical, Trenched and Asymmetrical Shaped Holes,” Ph.D. thesis, University of Central Florida, Orlando.
16. Wright, L. M., Gao, Z., Varvel, T. A., and Han, J.-C., “Assessment of Steady State PSP, TSP, and IR Measurement Techniques for Flat Plate Film Cooling,” Heat Transfer: Volume 3, ASME, 2005, pp. 37-46.
17. Kurits, I. and Norris, J. D., 2011, “Temperature-Sensitive Paint Calibration Methodology Developed at AEDC Tunnel 9,” AIAA 2011-851.
18. Schramm, J.M., Hannemann, K., Ozawa, H., Beck, W. and Klein, Ch., 2014, “Development of Temperature Sensitive Paints for the High Enthalpy Shock Tunnel Goettingen,” 8th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon.
19. Product catalog, 2017, Innovative Scientific Solutions Inc.
20. Jeziorek, Ł., 2017, “Rozwój Metodologii TSP (Farba Termoczuła) i Potencjału Badań Laboratoryjnych z Nią Związanych,” (ang. Development of Thermal Sensitive Paint Methodology and Its Research Capabilities), Sprawozdanie z pracy badawczej nr 2017/PS/01, Institute of Aviation, Warsaw.
21. Kercher, D.M., Tabakoff W., 1969, “Heat Transfer by a Square Array of Round Air Jets Impinging Perpendicular to a Flat Surface Including the Effect of Spent Air,” ASME paper 69-GT-4.
22. Floerschuetz, L.W., Metzger D.E., Truman C.R., 1981, “jet Array Impingement with Crossflow – correlation of streamwise Resolved Flow and Heat Transfer Distributions,” NASA Contractor Report 3373.
23. Chamberlain, J.E., 1966, “Heat Transfer Between a Turbulent Round Jet and a Segmented Plate Perpendicular to It,” M.Sc. thesis, Newark College of Engineering.
24. Szafran, K., Shcherbonos, O. and Ejmocki, D., 2014, “Effect of duct shape on ducted propeller trust performance,” Transactions of the Institute of Aviation, No. 4 (237), pp. 85-91.
25. Ruchała, P. and Szafran, K., 2016, ”Praktyczne Aspekty Zastoso-wania Otunelowanych Śmigieł Pchających,” (ang. The Aspects of Practical Application of Ducted Fans), Transactions of the Institute of Aviation, No. 3 (244), pp. 257-266.
26. Navarra, K. R., 1997, “Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications,” Ms.C. thesis, Virginia Polytechnic Institute and State University.
Published
2018-12-20
Issue
Section
Eksploatacja i Testy/Exploitation and Tests
Copyright (c) 2018 Autobusy – Technika, Eksploatacja, Systemy Transportowe
This work is licensed under a Creative Commons Attribution 4.0 International License.
