Other
Scientific paper
May 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980odu..rept.....k&link_type=abstract
Final Report, period ending 29 Feb. 1980 Old Dominion Univ., Norfolk, VA.
Other
Atmospheric Entry, Galileo Probe, Jupiter Atmosphere, Laminar Flow, Radiative Heat Transfer, Turbulent Flow, Ablation, Aerodynamic Heating, Axisymmetric Bodies, Finite Difference Theory, Heat Shielding, Phenols
Scientific paper
Laminar and turbulent flow-field solutions with coupled carbon-phenolic mass injection are presented for the forebody of a probe entering a nominal Jupiter atmosphere. Solutions are obtained for a 35-degree hyperboloid and for a 45-degree spherically blunted cone using a time-dependent, finite-difference method. The radiative heating rates for the coupled laminar flow are significantly reduced as compared to the corresponding no-blowing case; however, for the coupled turbulent flow, it is found that the surface radiative heating rates are substantially increased and often exceed the corresponding no-blowing values. Turbulence is found to have no effect on the surface radiative heating rates for the no-blowing solutions. The present results are compared with the other available solutions, and some additional solutions are presented.
Kumar Alok
Tiwari S. N.
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