[
[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] 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
[
[4] 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
[
[5] 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
[
[6] 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
[
[7] 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
[
[8] 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
[
[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] Wierciński, Z., Kaiser, M., Żabski, J., 2007, “Extended Reynolds Analogy for Different Flow Conditions of the Heated Plate,” Transactions of the Institute of Aviation, No. 2 (191), pp. 83-91.
]Search in Google Scholar
[
[11] 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
[
[12] 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
[
[13] 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
[
[14] 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
[
[15] Liu, Q., 1993, “Study of Heat Transfer Characteristics if Impinging Air Jet Using Pressure and Temperature Sensitive Luminescent Paint,” Ph.D. thesis, Nanjing University of Aeronautics and Astronautics.
]Search in Google Scholar
[
[16] 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
[
[17] 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
[
[18] 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
[
[19] 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
[
[20] Jeziorek, Ł., 2017, “Rozwój Metodologii TSP (Farba Termoczuła) i Potencjału Badań Laboratory-jnych 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
[
[21] Product catalog, 2017, Innovative Scientific Solutions Inc.
]Search in Google Scholar
