Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field
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Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field
Vol. 23, Issue 2, (2008)
作者机构:
北京航空航天大学 宇航学院,北京,100083
作者简介:
基金信息:
DOI:
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Published:2008
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CHEN Yang, GAO Fang, ZHANG Zhen-peng, et al. Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field[J]. 2008, 23(2).
DOI:
CHEN Yang, GAO Fang, ZHANG Zhen-peng, et al. Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field[J]. 2008, 23(2).DOI:
Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field
a finite volume model suitable for simulating pipe wall transient heat transfer was established by employing two-dimensional finite control volume grids in axisymmetric cylindrical coordinates which can deal with two boundary heat transfer conditions including convection and radiation.Variable thermophysical properties of wall material and multilayer or vacuum sandwich structure of pipe wall were also considered.The temperature field model is a natural extension of flow field modeling method.The union of both forms the finite volume model(FVM) of quasi one-dimensional compressible transient pipe flow
which is a uniform numerical system of flow and heat transfer.Furthermore
combing with throttling model of valve core
the model can be further developed to establish the flow field and temperature field models of common components in pipe system.The modeling and simulation of a certain liquid rocket engine test-bed LO2 tank pressurization system shows that the FVMhas a wide scope of application and good simulation precision.
Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅰ) Finite volume model of flow field
Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (Ⅱ) Numerical model and simulation results of pressurization system
Calculation of airfoil anti-icing/deicing characteristics based on water film flow and coupled heat transfer
Numerical simulation of ideal MHD equations using HLLC scheme
Boundary ghost cell method for gas heat radiation calculation of hypersonic re-entry spacecraft
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