NUMERICAL SIMULATION OF SUBSONIC AND TRANSONIC FLOW AROUND THIN SHELLS
Abstract
Numerical simulation of flow around a nose fairing half of a launch vehicle was carried out, aerodynamic characteristics of the model were calculated at subsonic and transonic flow velocities, the flow patterns around a thin shell were analyzed.
About the Authors
A. A. Dyadkin
ОАО "РКК "Энергия"
Russian Federation
Russian Federation
A. Yu. Lutsenko
МГТУ им. Н.Э. Баумана
Russian Federation
Russian Federation
D. K. Nazarova
МГТУ им. Н.Э. Баумана;
ОАО "РКК "Энергия"
Russian Federation
Russian Federation
References
1. Petrov K.P. Aehrodinamika raket [Aerodynamics missiles] Moscow. Mashinostroenie. 1977. 136 p.
2. Nikitin N.D. Razrabotka metoda rascheta i issledovaniya aehrodinamicheskikh kharakteristik stvorok golovnihkh obtekateleyj raket-nositeleyj: Diss. na soiskanie uch. step. kand. fiz.-mat. nauk. [Development of the method of calculation and the research of aerodynamic characteristics of wing fairing of carrier rocket] Moscow. 1998. 161 p.
3. Alabova N. P., Bryukhanov N.A., Dyadjkin A.A., Krihlov A.N., Simakova T.V. Rolj kompjyuternogo modelirovaniya i fizicheskogo ehksperimenta v issledovaniyakh aehrogazodinamiki raketno-kosmicheskikh sistem v processe proektirovaniya. Kosmicheskaya tekhnika i tekhnologii [The role of computer simulashion and physical experiments in research aerogasdynamics space rocket systems in the processes of design. Space technology and Technology] Moscow. 2014. № 3(6). PP. 14 – 21.
4. Gavriliouk V.N., Lipatnikov A.V., Kozlyaev A.N. et cet. Computation Modelling of the Combastion Problems with the use of "Aeroshape3D" // Numerical Technique, ISTS.94-d-27, 1994.
5. Beloshitsky A.V., Gerasimov Yu.I, Dyadkin A.A. et cet. The flight measurements of aerodynamics influencies to "Рrogress-M" spacecraft at the jettisoning of "Soyuz" launcher head fairings // Proc. 4th Europ Symp. Aerothermodynamics for Space Applications, 15-18 Oct. 2001. Сарua. Italy. ESA SP487. March 2002.
6. Jasak H., Jemcov A., Tukovic Z. ОреnFoam: A C++ Library for Complex Physics Simulations // International Workshop on Coupled Method in Numerical Dynamics, 19-21 Sep. 2007. Dubrovnic, Croatia.
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, № 6. PP. 620 – 631.
8. Kalugin V.T., Golubev A.G., Epikhin A.S., Michkin A.A. Vozmozhnosti primeneniya otkrihtogo paketa OpenFOAM dlya chislennogo modelirovaniya otrihvnihkh techeniyj pri do- i sverkhzvukovihkh skorostyakh obtekaniya letateljnihkh apparatov. Nauchnihyj Vestnik MGTU GA [Possible applications OpenFOAM package for numerical simulation of separated flows at SUBSONIC and supersonic flow around the aircraft. Scientific bulletin MSTUCA] Moscow/ 2014. № 199(1). PP. 23 – 30.
9. Marcantoni L.F.G., Tamagno J.P., Elaskar S.A. High speed flow simulation using OpenFoam // Mecánica Computacional Vol XXXI, 2012. PP. 2939 – 2959.
Review
For citations:
Dyadkin A.A., Lutsenko A.Yu., Nazarova D.K. NUMERICAL SIMULATION OF SUBSONIC AND TRANSONIC FLOW AROUND THIN SHELLS. Civil Aviation High Technologies. 2016;(223):45-50. (In Russ.)
Views:
591
Email this article 
