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scientific edition of Bauman MSTUSCIENCE & EDUCATIONBauman Moscow State Technical University. El № FS 77 - 48211. ISSN 1994-0408
Experimental and mathematical simulation of fairing aircraft with braking devices
# 11, November 2012 DOI: 10.7463/1112.0489665
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References 1. Kalugin V. T. Aerodinamika organov upravleniia poletom letatel'nykh apparatov [Aerodynamics of control surfaces of flight of aircraft]. Moscow, Bauman MSTU Publ., 2004. 688 p. 2. Shvets A.I., Shvets I.T. Gazodinamika blizhnego sleda [Gas dynamics of the near trace]. Kiev, Naukova dumka, 1976. 382 p. 3. Krasnov N.F. Osnovy aerodinamicheskogo rascheta [Fundamentals of aerodynamics calculations]. Moscow, Vysshaia shkola, 1981. 496 p. 4. Chang P.K. Control of Flow Separation: Energy Conservation, Operational Efficiency and Safety. McGraw-Hill Companies, 1976. 523 p. (Russ. ed.: Chzhen P. Upravlenie otryvom potoka: Ekonomichnost', effektivnost', bezopasnost'. Moscow, Mir, 1979. 552 p.). 5. Belov I.A., Isaev S.A. Modelirovanie turbulentnykh techenii [Simulation of turbulent flows]. St. Petersburg, BGTU Publ., 2001. 107 p. 6. Ferziger J.H., Peric M. Computational Methods for Fluid Dynamics. Springer-Verlag, Berlin, 2002. 423 p. http://dx.doi.org/10.1007/978-3-642-56026-2 7. Weller H.G., Tabor G., Jasak H., Fureby C. A tensorial approach to computational continuum mechanics using object oriented techniques. Computers in Physics, 1998, vol. 12, no. 6, pp. 620-631. http://dx.doi.org/10.1063/1.168744 8. Jasak H., Weller H.G., Gosman A.D. High resolution NVD differencing scheme for arbitrarily unstructured meshes. Int. J. Numer. Meth. Fluids, 1999, vol. 31, no. 2, pp. 431-449. DOI: 10.1002/(SICI)1097-0363(19990930)31:2<431::AID-FLD884>3.0.CO;2-T 9. Fletcher C.A.J. Computational Techniques for Fluid Dynamics. In 2 vols. Vol. 1. Fundamental and General Techniques. Springer-Verlag, Berlin, 1988. (Russ. ed.: Fletcher K. Vychislitel'nye metody v dinamike zhidkostei. V 2 t. T.1. Osnovnye polozheniia i obshchie metody. Moscow, Mir, 1991. 504 p.). 10. Wyborny W., Kabelitz H.R. Comparison of hypersonic aerodynamic deceleration system based on gun tunnel investigations. AIAA Paper, 1970, no. 1174, 11 p. Publications with keywords: mathematical model, equations, turbulence model, braking devices, disc pads, bottom pressure Publications with words: mathematical model, equations, turbulence model, braking devices, disc pads, bottom pressure See also: Thematic rubrics: Поделиться:
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