Unsteady viscous vortex with flow toward the center
Strong unsteady viscous vortex of annular region, with tangential and radial flow, and core region with uniform axial flow toward center
Engineering topics
Publications and source records attributed to Deissler, R. G..
Strong unsteady viscous vortex of annular region, with tangential and radial flow, and core region with uniform axial flow toward center
Uniform longitudinal strain rate effect on weak homogeneous turbulence in compressible flow
Second order slip flow for rarefied gases, showing effect on velocity and temperature jumps at wall
Radiative diffusion in nongray gas with jump boundary condition
Equations for inhomogeneous turbulence constructed from Navier-Stokes and energy equations
Derivation of two-point correlation and spectral equations from equations of fluid and electrodynamics for mhd turbulence with uniform imposed magnetic field
Radiative diffusion in a nongray gas with jump boundary conditions
Turbulent heat transfer and temperature fluctuations in a field with uniform velocity and temperature gradients
Reference temperatures for turbulent, variable- property heat transfer in a tube for air, helium, argon, hydrogen and carbon dioxide
Effect on turbulence of buoyancy caused by vertical body force and temperature gradient
Pressure fluctuations in a weak turbulent field with a uniform transverse velocity gradient
Velocity and temperature correlation in homogeneous turbulent field
Effects of heterogeneity and of shear flow in weak turbulent fields
Turbulent forced convection heat transfer computations for air, helium, argon, hydrogen, and carbon dioxide
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A previous analysis of turbulent heat transfer and flow with variable fluid properties in smooth passages is extended to flow over a flat plate at high Mach numbers, and the results are compared with experimental data. Velocity and temperature distributions are calculated for a boundary layer with appreciative effects of frictional heating and external heat transfer. Viscosity and thermal conductivity are assumed to vary as a power or the temperature, while Prandtl number and specific heat are taken as constant. Skin-friction and heat-transfer coefficients are calculated and compared with the incompressible values. The rate of boundary-layer growth is obtained for various Mach numbers.
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