À propos de cet article

Citez

[1] Liu, T. and Sullivan, J.P., 2005, Pressure and Temperature Sensitive Paints, Springer, New York. Search in Google Scholar

[2] Jahanmiri, M., 2011, “Pressure Sensitive Paints: The Basics & Applications,” 2011:07, Chalmers University of Technology, Göteborg, Sweden. Search in Google Scholar

[3] Cottingham, T., 2015, “Characterization and Optimization of Temperature-Sensitive Microbeads for Simultaneous Thermometry and Velocimetry for Fluid Dynamic Applications,” M.Sc. thesis, University of Washington. Search in Google Scholar

[4] Kurits, I. and Norris, J. D., 2011, “Temperature-Sensitive Paint Calibration Methodology Developed at AEDC Tunnel 9,” AIAA 2011-851.10.2514/6.2011-851 Search in Google Scholar

[5] 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. Search in Google Scholar

[6] 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. 85-91.10.5604/05096669.1151026 Search in Google Scholar

[7] Ruchała, P. and Szafran, K., 2016, “Praktyczne Aspekty Zastosowania Otunelowanych Śmigieł Pchających,” (ang. The Aspects of Practical Application of Ducted Fans), Transactions of the Institute of Aviation, No. 3 (244), pp. 257-266.10.5604/05096669.1226158 Search in Google Scholar

[8] Navarra, K. R., 1997, “Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications,” Ms.C. thesis, Virginia Polytechnic Institute and State University. Search in Google Scholar

[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. Search in Google Scholar

[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. 15-24.10.1051/eucass/201203015 Search in Google Scholar

[11] Rosłowicz, A. and Bednarczyk, P., 2017, “Analysis of Heat Transfer in a Supersonic Rocket Head,” Transactions of the Institute of Aviation, No. 1 (246), pp.79-94.10.2478/tar-2017-0008 Search in Google Scholar

[12] Zuniga, H. A., 2009, “Study of Film Cooling Effectiveness: Conical, Trenched and Asymmetrical Shaped Holes,” Ph.D. thesis, University of Central Florida, Orlando. Search in Google Scholar

[13] 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. 37-46.10.1115/HT2005-72363 Search in Google Scholar

[14] Crafton, J.W., 2004, “The Impingement of Sonic and Sub-Sonic Jets onto a Flat Plate at Inclined Angles,” Ph.D. Thesis, Purdue University. Search in Google Scholar

[15] Crafton, J., Ladchenko, N., Guille, M. and Sullivan, P., “Application of Temperature and Pressure Sensitive Paint to an Obliquely Impinging Jet,” 37th Aerospace Sciences Meeting and Exhibit, AIAA-99-0387, Reno, USA. Search in Google Scholar

[16] Bell, J.H., 2004, “Applications of Pressure-sensitive Paint to Testing at Very Low Flow Speeds,” AIAA-2004-0878.10.2514/6.2004-878 Search in Google Scholar

[17] 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. Search in Google Scholar

[18] Liu, Q., 1993, “Study of Heat Transfer Characteristics if Impinging Air Jet Using Pressure and Temperature Sensitive Search in Google Scholar

[19] Gao, L., 2003, “Effect of Jet Hole Arrays Arrangement on Impingement Heat Transfer,” M.Sc. thesis, Louisiana State University. Search in Google Scholar

[20] Sullivan, J., 2009, “Molecular Sensors – Temperature Sensitive Paint”, https://slideplayer.com/slide/1675994/LuminescentPaint,” Ph.D. thesis, Nanjing University of Aeronautics and Astronautics. Search in Google Scholar

[21] 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. Search in Google Scholar

eISSN:
2545-2835
Langue:
Anglais
Périodicité:
4 fois par an
Sujets de la revue:
Engineering, Introductions and Overviews, other, Geosciences, Materials Sciences, Physics