Calculation of a nonequilibrium viscous shock layer with allowance for coupled heat transfer

1984 ◽  
Vol 19 (2) ◽  
pp. 297-303 ◽  
Author(s):  
V. I. Zinchenko ◽  
S. I. Pyrkh
Keyword(s):  
Heat Transfer ◽  
Shock Layer ◽  
Viscous Shock Layer ◽  
Coupled Heat Transfer

Hypersonic Viscous Shock Layer Calculation of Leeward Vortex-Induced Heat Transfer on a Sharp Cone at a High Angle of Attack

1977 ◽  
Vol 99 (2) ◽  
pp. 307-313 ◽  
Author(s):  
J. C. Adams
Keyword(s):  
Heat Transfer ◽  
Flow Field ◽  
Shock Layer ◽  
Vortex Flow ◽  
Local Heating ◽  
Three Dimensional ◽  
Leeward Side ◽  
Heating Rates ◽  
Viscous Shock Layer ◽  
Sharp Cone

An analysis technique applicable to the problem of leeward vortex-induced heat transfer on a sharp cone at high angles of incidence under hypersonic laminar flow conditions is presented. The analysis, a three-dimensional hypersonic viscous shock layer approach in conjunction with a numerical solution procedure, is shown to be both applicable and accurate based on comparisons of heat-transfer distributions, surface pressure distributions, and leeward meridian flow-field profile measurements taken in a hypersonic wind tunnel. Detailed calculations of the embedded vortex flow field on the leeward side of the cone are presented in such a manner as to clearly portray exactly how embedded vortex flow influences local heating rates.

Nonequilibrium Viscous Shock-Layer Heat Transfer with Arbitrary Surface Catalycity

2005 ◽  
Vol 42 (2) ◽  
pp. 193-200 ◽  
Author(s):  
George R. Inger ◽  
Richard L. Baker
Keyword(s):  
Heat Transfer ◽  
Shock Layer ◽  
Viscous Shock Layer

scholarly journals Coupled heat transfer between a viscous shock gasdynamic layer and a transversely streamlined anisotropic half-space

2020 ◽  
Vol 12 (S) ◽  
pp. 211-220
Author(s):  
Olga V. TUSHAVINA
Keyword(s):  
Heat Transfer ◽  
Thermal Conductivity ◽  
Boundary Condition ◽  
Analytical Solution ◽  
Half Space ◽  
Stokes Equations ◽  
Conjugate Problem ◽  
Viscous Shock Layer ◽  
Boundary Layer Equations ◽  
Coupled Heat Transfer

The purpose of the article is to analytically solve the conjugate problem of heat transfer in a viscous shock layer on a blunt object and thermal conductivity in an anisotropic half-space. A feature of the flow around such bodies near the critical point is that in this case, the boundary layer equations are not satisfied and it is necessary to solve the Navier-Stokes equations together with the equations of continuity, state, and energy, however, in a stationary formulation of an incompressible flow. The problem of coupled heat transfer between a viscous shock gasdynamic layer and anisotropic half-space with the assumption of incompressibility of the gasdynamic flow behind the normal part of the shock wave is posed. An analytical solution to this problem is obtained with a boundary condition at the gas-solid object interface in the form of a parameter – temperature, as well as an analytical solution to the thermal conductivity problem in an anisotropic half-space with the same boundary condition.

Higher-order viscous shock-layer solutions for high altitude flows

1993 ◽  
Author(s):  
ROOP GUPTA ◽  
SUDHEER NAYANI ◽  
KAM-PUI LEE ◽  
ERNEST ZOBY
Keyword(s):  
High Altitude ◽  
Shock Layer ◽  
Higher Order ◽  
Viscous Shock Layer
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