Email this article 
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
- Authors: Ivanov I.1, Kryukov I.2, Shustov S.3
-
Affiliations:
- Moscow State University named after M.V. Lomonosov
- Institute for Problems in Mechanics named after A.J. Ishlinsky
- Samara State Aerospace University
- Issue: Vol 13, No 1 (2014)
- Pages: 112-122
- Section: MECHANICAL ENGINEERING AND POWER ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1703
- DOI: https://doi.org/10.18287/1998-6629-2014-0-1(43)-112-122
- ID: 1703
Cite item
Full Text
Abstract
The paper presents the statement of the problem of numerical simulation of gas dynamics of nozzles and jets of small-dimensioned gas generators of supersonic flows based on boundary layer and Navier-Stokes equations and the results of solving it. The results of the numerical studies of gas dynamics of nozzles and jets for standard small-dimensioned gas generators with a thrust 6 N and 12 N are given. Significant potential of increasing specific impulse by optimizing the contour of supersonic nozzles of small-dimensioned gas generators are exhibited. The process of shock wave formation in the supersonic part of the nozzle of a standard smalldimensioned gas generator is numerically investigated. Significant impact of shock waves on the gas dynamics of vacuum jets is illustrated.
About the authors
I. Ivanov
Moscow State University named after M.V. Lomonosov
Author for correspondence.
Email: ivanovmai@mail.ru
Candidate of Science (Phys.&Math.)
Associate Professor Faculty of Physics
Russian FederationI. Kryukov
Institute for Problems in Mechanics named after A.J. Ishlinsky
Email: ikryukov@gmail.com
Candidate of Science (Phys.&Math.)
Senior Research Fellow
Russian FederationS. Shustov
Samara State Aerospace University
Email: shustov.st@yandex.ru
Candidate of Science (Engineering), Associate Professor
Department of Theory of Aircraft Engines
Russian FederationReferences
- Byrkin A.P. Numeral calculation of an axisymmetric laminar boundary layer with regard to transverse curvature // Trudy TsAGI, is. 1035. Moscow, 1966. 20 p. (In Russ)
- Avduevsky V.S., Kopyatkevich R.M. Calculation of laminar boundary layer in compressed gas in the presence of heat exchange and arbitrary pressure distribution along the surface // Izvestiya ANSSSR, OTN, Mekhanika and mashinostroenie. 1960. 1. P. 3-11. (In Russ.)
- Shustov S.A. Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip // Vestnik Samarskogo gosudarstvennogo aerokosmicheskogo universiteta. 2009. No. 1(17). P. 79-89. (In Russ.)
- Avduevsky V.S. etc. Osnovy teploperedachi v aviatsionnoy i raketno-kosmicheskoy tekhnike [Fundamentals of heat transfer in aircraft and space-rocket engineering]. Moscow: Mashinostroenie Publ., 1975. 645 p.
- Shustov S.A. Methods and results of selecting an optimal contour of supersonic nozzles in low-thrust rocket engines // Proceedings of NPNJ-2012, 25-31 May 2012, Аlushta. М.: Publishing house MAI-PRINT, 2012, p.66-68.(In Russ.)
- Melnikov D.A., Pirumov U.G., Sergienko A.A. Nozzles of jet engines. In the book: Aeromekhanika i gazovaya dinamika [Aerodynamics and gas dynamics]. Мoscow: Nauka Publ., 1976. P. 57-75.
- Glushko G.S., Ivanov I.E., Kryukov I.A. Calculational method for turbulent supersonic flows // Matematicheskoe modelirovanie. 2009. V. 21, № 12. P. 103-121. (In Russ.)
Supplementary files
