Using multilayer neural networks in determination of pressure on the surface of supersonic flying vehicles-Reference-Cited by-同舟云学术

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Using multilayer neural networks in determination of pressure on the surface of supersonic flying vehicles

Published:2019 Issue: Volume: Page:
ISSN:0094-243X
Container-title:XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration
language:
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Author:

Sapozhnikov D. A.,Bulgakov V. N.,Kotenev V. P.,Ratslav R. A.,Kozyrev N. M.

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5133251

Reference20 articles.

1. Tucker, P. G. (2016). Advanced computational fluid and aerodynamics (Vol. 54). Cambridge University Press.

2. Krasnov, N. F., & Morris, D. N. (1970). Aerodynamics of bodies of revolution (Vol. 455, No. PR). RAND CORP SANTA MONICA CALIF.

3. Lunev, V. V. (2009). Real gas flows with high velocities. CRC Press.

4. Aerodynamic Characteristics at Low Reynolds Number for Wings of Various Planforms

5. High-Resolution Reynolds-Averaged Navier-Stokes Flow Predictions over Axisymmetric Bodies with Tapered Tails

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Research of the proportional valve effective area dependence on the control signal and the differential pressure;XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2021

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