@article{bynum_hollis_hassan_xiao_2008, title={Turbulent aeroheating on the mars science laboratory entry vehicle}, volume={22}, ISSN={["1533-6808"]}, DOI={10.2514/1.33281}, abstractNote={A series of calculations are carried out for a Mars Science Laboratory entry vehicle heat shield and compared with tests carried out in the Arnold Engineering Development Center for Mach 8 and 10 and a range of Reynolds numbers. Three turbulence models are employed that are implemented in the LAURA code: the Cebeci-Smith algebraic model, the 98 Wilcox k − ω model, and the k − ζ model. In general, good agreement is indicated with turbulent predictions. Because the flow is attached, the algebraic model performs as well as other models.}, number={2}, journal={JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER}, author={Bynum, Michael D. and Hollis, Brian R. and Hassan, H. A. and Xiao, X.}, year={2008}, pages={306–309} }