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Development of an Engine Anti-Ice Protection System using Experimental and Numerical Approaches
Technical Paper
2007-01-3355
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This paper describes part of the process of development of engine inlet anti-ice system, based on numerical simulation and icing wind tunnel tests. A number of critical cases are selected spanning the Appendix C. At these selected points, a set of tools for thermal analysis is applied and different piccolo tubes designs are analyzed. The selected configurations and conditions are tested in an Icing Wind Tunnel, where the piccolo flow parameters are optimized and data is collected to establish a basis for validation of the numerical tools. Using the experimental data, a high fidelity set of thermal analysis tools is validated, which can be used to explore the whole design space of system in order to refine the design for a second iteration (if necessary). The comparison of numerical and experimental data has shown the validity and accuracy of the procedure.
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Domingos, R., Pustelnik, M., Trapp, L., Lima da Silva, G. et al., "Development of an Engine Anti-Ice Protection System using Experimental and Numerical Approaches," SAE Technical Paper 2007-01-3355, 2007, https://doi.org/10.4271/2007-01-3355.Also In
References
- Dezitter, F. Chene, G. Viala, S. Calmels, B. 3D Ice Accretion and Aerodynamic Penalties Prediction on Aircraft 2003-3883 16 th AIAA Computational Fluid Dynamics Conference 23-26 June 2003 Orlando, FL, USA
- Silveira, R. Maliska, C. R. Numerical Simulation of Ice Accretion on the Leading Edge of Aerodynamic Profiles th International Congress of Mechanical Engineering (COBEM), XX Brazil
- Goldstein, R. J. Behbahni, A. I. Heppelman, K. K. “Streamwise Distribution of the Recovery Factor and the Local Heat Transfer Coefficient to an Impinging Circular Air Jet,” Intl. J. of Heat and Mass Trans. 29 8 1227 1235 1986
- Wright, W. B. An Evaluation of Jet Impingement Heat Transfer Correlations for Piccolo Tube Application 42 nd AIAA Aerospace Sciences meeting and Exhibit 5-8 January 2004 Reno, NV, USA
- Wirogo, S. Srirambhatla, S. An Eulerian Method to Calculate the Collection Efficiency on Two and Three Dimensional Bodies 2003-1073 41 st Aerospace sciences Meeting and Exhibit 6-9 January 2003 Reno, NV, USA
- Anderson, D. N. Manual of Scaling Methods NASA CR-2004-212875 March 2004 Brook Park, Ohio, USA