Geodesic
Experimental data completing by numerical simulation of flow around supersonic passenger aircraft structural
Matematičeskoe modelirovanie, Tome 27 (2015) no. 3, pp. 121-136

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The review of aerodynamical characteristics for perspective passenger supersonic aircraft investigation main methods is presented. Obtaining of numerical and experimental methodologies are described. The methodology for correct comparison of wind tunnel model with duct and real aircraft with working engine in free flow conditions is considered. The resumes about possibility of missing experimental completing by numerical simulation are formulated.
Keywords: numerical simulation, numerical and experimental data comparison, business supersonic aircraft.
Mots-clés : program validation 
@article{MM_2015_27_3_a8,
     author = {K. Anisimov and S. Kalashnikov},
     title = {Experimental data completing by numerical simulation of flow around supersonic passenger aircraft structural},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {121--136},
     publisher = {mathdoc},
     volume = {27},
     number = {3},
     year = {2015},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2015_27_3_a8/}
}
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K. Anisimov; S. Kalashnikov. Experimental data completing by numerical simulation of flow around supersonic passenger aircraft structural. Matematičeskoe modelirovanie, Tome 27 (2015) no. 3, pp. 121-136. http://geodesic.mathdoc.fr/item/MM_2015_27_3_a8/