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Heat Transfer Determined by the Temperature Sensitive Paint Method

Calibration Methodology Developed at AEDC Tunnel 9,” AIAA 2011-851. [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,” 8 th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon. [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. [7] Ruchała, P. and Szafran, K., 2016, “Praktyczne Aspekty

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Temperature Measurements using Thermal Sensitive Paint

, “Development of Temperature Sensitive Paints for the High Enthalpy Shock Tunnel Goettingen,” 8th European Symposium on Aerothermodynamics for Space Vehicles, Lissabon. [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] Wierciński, Z., Kaiser, M., Żabski, J., 2007, “Extended Reynolds Analogy for Different Flow Conditions of the Heated Plate,” Transactions of the

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Improvement and Optimisation of Gyroplane Performance

Decennial Specialists’ Conference on Aeromechanics, San Francisco, California, 21th - 23th January, 2004. [7] Harwood P., Flying ‘New Generation’ Gyrocopter, A guide for converting pilots! http://www.gyrocopterschool.com/gyrocopter-autogyro-gyroplane/how-to-fly-gyros/ [8] http://airfoiltools.com/airfoil/details?airfoil=n8h12-il [9] http://wirnikautorotacyjny.pl/ , website of the project “Modern Gyroplane Main Rotor”, (UDA-POIG.01.03.01-14-007/12), co-financed by the European Regional Development Fund under the Operational Programme Innovative Economy

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