Abstract
A finite difference method is proposed for solving the simplified Navier-Stokes equations for the case of a supersonic laminar off-design jet issuing into a parallel supersonic stream. Calculations are made of underexpanded and overexpanded jets for various Reynolds numbers.
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Abbreviations
- M:
-
Mach number
- R:
-
Reynolds number
- R:
-
(ρur)/μ
- P:
-
Prandtl number
- p:
-
pressure
- ρ:
-
density
- T:
-
temperature
- u:
-
longitudinal velocity component
- v:
-
transverse velocity component
- r:
-
characteristic initial jet radius
- μ:
-
viscosity
- λ:
-
thermal conductivity
- 1:
-
flow parameters on jet axis at initial section
- 2:
-
outer undisturbed stream
References
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V. M. Emel'yanov, “Calculation of axisymmetric supersonic jet flowing into a supersonic wake or a stationary medium”, Inzh. zh. [Soviet Engineering Journal], vol. 5, no. 3, 1965.
G. N. Abramovich, Theory of Turbulent Jets [in Russian], Fizmatgiz, Moscow, 1960.
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I. Yu. Brailovskaya and L. A. Chudov, “Solution of the boundary layer equation by a difference method”, collection: Computational Methods and Programming [in Russian], Izd-vo MGU, Sb. rabot Vychisl. tsentra Mosk. un-ta, no. 1, 1962.
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Bondarev, E.N., Gorina, A.N. Solution of the problem of the supersonic laminar off-design jet in a parallel flow using a difference method. Fluid Dyn 3, 76–78 (1968). https://doi.org/10.1007/BF01019200
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DOI: https://doi.org/10.1007/BF01019200