Conjugate Heat Transfer Study in Hypersonic Flows
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Abstract
Coupled and decoupled conjugate heat transfer (CHT) studies are carried out to imitate experimental studies for heat transfer measurement in hypersonic flow regime. The finite volume based solvers are used for analyzing the heat interaction between fluid and solid domains. Temperature and surface heat flux signals are predicted by both coupled and decoupled CHT analysis techniques for hypersonic Mach numbers. These two methodologies are also used to study the effect of different wall materials on surface parameters. Effectiveness of these CHT solvers has been verified for the inverse problem of wall heat flux recovery using various techniques reported in the literature. Both coupled and decoupled CHT techniques are seen to be equally useful for prediction of local temperature and heat flux signals prior to the experiments in hypersonic flows.
Keywords
Finite volume method Hypersonic flow Conjugate heat transferNotations
- C
Specific heat at constant, kJ/kg K
- E
Total specific energy, kJ/kg
- e
Specific internal energy, kJ/kg
- H
Total specific enthalpy, kJ/kg
- h
Specific enthalpy, kJ/kg
- k
Thermal conductivity, W/m K
- L
Length, m
- M
Mach number
- p
Pressure, N/m2
- \({\dot{\text{q}}}\)
Heat flux, W/m2
- Pr
Prandtl number
- R
Universal gas constant
- Re
Reynolds number
- S
Source term
- s
Sutherland’s constant
- St
Stanton Number
- T
Temperature, °C
- u
X-direction velocity, m/s
- v
Y-direction velocity, m/s
- x, y
Cartesian co-ordinate system
Greek symbols
- λ
Courant number
- γ
Specific heat ratio
- μ
Dynamic viscosity, kg/ms
- τ
Shear stress, N/m2
- ρ
Density, kg/m3
- δ
A parameter in AUSM-δ scheme
Subscripts
- ∞
Freestream quantities
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