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Performance of Entry Heat Shields on Pioneer Venus Probes
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Measurements of Thermal Structure and Thermal Contrasts in the Atmosphere of Venus and Related Dynamical Observations; Results fromthe Four Pioneer Venus Probes
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No. Dec. 30
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Seiff, A., Kirk, D. B., Young, R. E., Blanchard, R. C., Findlay, J. T., Kelly, G. M., and Sommer, S. C., "Measurements of Thermal Structure and Thermal Contrasts in the Atmosphere of Venus and Related Dynamical Observations; Results fromthe Four Pioneer Venus Probes," Journal of Geophysical Research, Vol. 85, No. A13, Dec. 30, 1980, pp7903-7933.
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Analysis of the Heat-Shield Experiment on the Pioneer-Venus Entry Probes
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July 14-16
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Wakefield, R.M.1
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Galileo Probe Heat Shield Ablation Experiment
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Survey of the Supporting Research and Technology for Thermal Protection for the Galileo Probe
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Aerothermal Environment for the Pioneer Venus Multiprobe Mission
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Progress in Astronautics and Aeronautics
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Approximate Convective Heating Equations for Hypersonic Flows
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A Study of the Aerothermal Entry Environment For the Galileo Probe
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The Effect of Modeled Turbulence on a Hypersonic Shock Layer with Massive Ablation Injectin
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Menees, G. P., Lombard, C. K., "The Effect of Modeled Turbulence on a Hypersonic Shock Layer with Massive Ablation Injectin," AIAA paper 811071, June 23-25, 1981.
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An Evaluation of Turbulence Models for Massively Blown Surfaces
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June 7-11
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Gupta, R. N., Moss, J. N., Zoby, E. V., and Simmonds, A. L., "An Evaluation of Turbulence Models for Massively Blown Surfaces," AIAA paper 82-0875, June 7-11, 1982.
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Injection-Induced Turbulence in Stagnation-Point Boundary Layers
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Feb
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Park, C., "Injection-Induced Turbulence in Stagnation-Point Boundary Layers," AIAA journal, Vol. 22, No. 2, Feb. 1984, pp219-225.
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Preliminary Study of the MUSES-C Reentry
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Ahn, H. K., and Park. C., "Preliminary Study of the MUSES-C Reentry," AIAA paper 97-0278, January 1997.
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A Pointwise Version of Baldwin-Barth Turbulence Model
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A Flux Splitting Scheme with High-Resolution and Robustness for Discontinuities
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An LU-SSOR scheme for the Euler and Navier-Stokes Equations
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Basic Governing Equatiohs for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles
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The Computation of Weakly Ionized Hypersonic Flows in Thermo-Chemical Nonequilibrium
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Stanford University
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Dynamics of Pyrolysis Gas in Charring Materials Ablation
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January
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Ahn, H. K., Park, C., and Sawada, K., "Dynamics of Pyrolysis Gas in Charring Materials Ablation," AIAA paper 98-0165, January 1998.
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Stagnation-Point Heat Transfer Rates for Pioneer-Venus Probes
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January
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Park, C, and Ahn, H. K., "Stagnation-Point Heat Transfer Rates for Pioneer-Venus Probes," AIAA paper 98-0832, January 1998.
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A Viscosity Equation for Gas Mixtures
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A Review of Reaction Rates and Thermodynamic and Transport Properties for an 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30000 K
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Numerical Simulation of Hypersonic Flow over a Sphere with Surface Injection
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Dendou, E., and Sawada, K. "Numerical Simulation of Hypersonic Flow over a Sphere with Surface Injection," AIAA paper 98-0773, January 1998.
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