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Su, F. Y.

Publications and source records attributed to Su, F. Y..

6 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1972

Radiative transfer effects on reflected shock waves. II - Absorbing gas.

Radiative cooling effects behind a reflected shock wave are calculated for an absorbing-emitting gas by means of an expansion procedure in the small density ratio across the shock front. For a gray gas shock layer with an optical thickness of order unity or less the absorption integral is simplified by use of the local temperature approximation, whereas for larger optical thicknesses a Rosseland diffusion type of solution is matched with the local temperature approximation solution. The calculations show that the shock wave will attenuate at first and then accelerate to a constant velocity. Under appropriate conditions the gas enthalpy near the wall may increase at intermediate times before ultimately decreasing to zero. A two-band absorption model yields end-wall radiant-heat fluxes which agree well with available shock-tube measurements.

Su, F. Y.↗
NASA NTRS1972

The radiative budget for polluted layers in the stratosphere.

A simple, yet physically realistic, six-step nongray radiative model of the atmosphere is applied to a parametric study aimed at a preliminary assessment of the radiative effects of a water-vapor and a carbon-dioxide layer injected into the lower stratosphere by the exhaust gases of supersonic (SST) and hypersonic (HST) transport aircraft. The fundamental differences between the effects of a pure water-vapor layer and a pure carbon dioxide layer are demonstrated. It is shown that with a water-vapor layer the earth's surface temperature will decrease and, for conditions appropriate for the SST, will change by a few hundredths of a degree. Within the layer, the temperature will increase on the order of one degree. For the HST, the radiative effects are shown to be roughly ten times greater than for the SST.

Su, F. Y.↗
NASA NTRS1971

Radiative transfer effects on reflected shock waves. I - Transparent gas.

Analytical and numerical calculation of the effects of radiative cooling on the flow field and heat transfer behind a reflected shock wave. The analytical solutions are developed by an expansion procedure about the Newtonian limit - i.e., the flow variables are expanded in the small parameter epsilon representing the initial density ratio across the shock front. Solutions carried out through the zeroth- and first-orders in epsilon show an accuracy to the order of epsilon squared - namely, for the specific conditions considered the analytically calculated enthalpy changes agree to within 2% with the numerically computed changes. The numerical procedure consists of a finite-difference calculation with pressure gradients neglected. The analytical calculations show that pressure-gradient effects may be neglected, except at very long times when the shocked gas has cooled by a large amount. The present calculations show much greater shock-wave attenuation than does a previous numerical computation. This difference is attributed to a better representation of the thermodynamic properties in the present calculations.

Su, F. Y.↗