2014
DOI: 10.1016/j.actaastro.2014.06.036
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Hypersonic static aerodynamics for Mars science laboratory entry capsule

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Cited by 10 publications
(1 citation statement)
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“…Secondly, previous turbulent heating augmentation (turbulent heat flux above laminar) and transition onset correlations, which can be employed as engineering-level design and analysis tools, were fitted by hypersonic wind-tunnel data of scaled 70 o sphere-cone models [14,20]. Unfortunately, no ground-based experiments can fully reproduce the high-speed and high-temperature Martian flow occurring at real flight conditions [21]. Besides, the effects of sphere-cone angle were not included in these correlations.…”
Section: Accepted Manuscriptmentioning
confidence: 99%
“…Secondly, previous turbulent heating augmentation (turbulent heat flux above laminar) and transition onset correlations, which can be employed as engineering-level design and analysis tools, were fitted by hypersonic wind-tunnel data of scaled 70 o sphere-cone models [14,20]. Unfortunately, no ground-based experiments can fully reproduce the high-speed and high-temperature Martian flow occurring at real flight conditions [21]. Besides, the effects of sphere-cone angle were not included in these correlations.…”
Section: Accepted Manuscriptmentioning
confidence: 99%