The paper presents a multi-purpose computational system SMILE based on statistical methods of computational rarefied gas dynamics and aimed at the study of different aerodynamic problems in regimes from free molecular through transitional to continuum. The results of application of SMILE to investigation of flows about X38 model geometry, reentry capsule Soyuz, and space station Mir are presented. An engineering approach based on local bridging is also used to calculate aerodynamic characteristics of Soyuz and Mir in free molecular and transitional regimes.
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Univ Michigan, Anthropol, Ann Arbor, MI 48109 USA
Univ Michigan, Environm Hlth Sci, Ann Arbor, MI 48109 USAUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Childebayeva, Ainash
Dolinoy, Dana C.
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Univ Michigan, Environm Hlth Sci, Ann Arbor, MI 48109 USA
Univ Michigan, Nutr, Ann Arbor, MI 48109 USAUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Dolinoy, Dana C.
Goodrich, Jaclyn M.
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Univ Michigan, Environm Hlth Sci, Ann Arbor, MI 48109 USAUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Goodrich, Jaclyn M.
Rivera-Chira, Maria
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Univ Peruana Cayetano Heredia, Dept Ciencias Biol & Fisiol, Lima, PeruUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Rivera-Chira, Maria
Leon-Velarde, Fabiola
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Univ Peruana Cayetano Heredia, Dept Ciencias Biol & Fisiol, Lima, PeruUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Leon-Velarde, Fabiola
Kiyamu, Melisa
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Univ Peruana Cayetano Heredia, Dept Ciencias Biol & Fisiol, Lima, PeruUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Kiyamu, Melisa
Brutsaert, Tom D.
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Syracuse Univ, Exercise Sci, Syracuse, NY 13244 USAUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA
Brutsaert, Tom D.
Bigham, Abigail W.
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Univ Michigan, Anthropol, Ann Arbor, MI 48109 USAUniv Michigan, Anthropol, Ann Arbor, MI 48109 USA