Completion of the experimental data by mathematical simulation of a flow around the structural elements of a supersonic passenger aircraft

Author:

Anisimov K. S.,Kalashnikov S. V.

Publisher

Pleiades Publishing Ltd

Subject

Computational Mathematics,Modeling and Simulation

Reference23 articles.

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2. S. A. Glazkov, A. R. Gorbushin, V. V. Vlasenko, A. I. Ivanov, A. V. Semenov, and J. Quest, “Numerical and experimental investigations of slot flow with respect to wind tunnel wall interference assessment,” in Proceedings of the 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, June 28, 2004, Portland, Oregon.

3. A. R. Gorbushin, N. N. Khoziaenko, T. V. Konotop, and V. A. Terekhin, “Investigation of the rear support interference on the aerodynamic characteristics of the RRJ-95 model in the T-128 transonic wind tunnel,” in Proceedings of the 21st International Congress on Instrumentation in Aerospace Simulation Facilities, Aug. 29–Sept. 1, 2005, Sendai International Center, Sendai, Japan.

4. S. M. Bosnyakov, V. V. Vlasenko, I. A. Kursakov, S. V. Mikhailov, and J. Quest, “A problem of interference between ogival body of revolution and wind tunnel sting and peculiarities of its solution using computers,” Uch. Zap. TsAGI, No. 3, 25 (2011).

5. V. G. Blishch, “On external and internal aerodynamical forces and moments of flight vehicles with air-breathing engines and their models at incidence and sideslip,” Tr. TsAGI, No. 2328, 1 (1987).

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1. Conceptual aerodynamic design of an executive supersonic passenger aircraft – ESPA;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-06-07

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