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This article is cited in 1 scientific paper (total in 1 paper)
Experimental data completing by numerical simulation of flow around supersonic passenger aircraft structural
K. Anisimova, S. Kalashnikovb a Moscow Institute of Physics and Technology (State University)
b Zhukovsky Central Aerohydrodynamic Institute (TsAGI)
Abstract:
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, program validation, numerical and experimental data comparison, business supersonic aircraft.
Received: 20.11.2013
Citation:
K. Anisimov, S. Kalashnikov, “Experimental data completing by numerical simulation of flow around supersonic passenger aircraft structural”, Matem. Mod., 27:3 (2015), 121–136; Math. Models Comput. Simul., 7:5 (2015), 495–505
Linking options:
https://www.mathnet.ru/eng/mm3586 https://www.mathnet.ru/eng/mm/v27/i3/p121
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Abstract page: | 375 | Full-text PDF : | 129 | References: | 47 | First page: | 21 |
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