Geodesic
Study of supersonic flow past segmental and conical bodies with allowance for chemical reactions
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 45 (2005) no. 11, pp. 2070-2076

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A numerical method was developed for computing three-dimensional flows past segmental and conical blunt bodies with allowance for equilibrium chemical reactions in the shock layer. The aerodynamic characteristics and flow fields were computed along the trajectory of space vehicles descending in the Martian and Terrestrial atmospheres. 
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     author = {M. M. Golomazov},
     title = {Study of supersonic flow past segmental and conical bodies with allowance for chemical reactions},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {2070--2076},
     publisher = {mathdoc},
     volume = {45},
     number = {11},
     year = {2005},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_2005_45_11_a14/}
}
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M. M. Golomazov. Study of supersonic flow past segmental and conical bodies with allowance for chemical reactions. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 45 (2005) no. 11, pp. 2070-2076. http://geodesic.mathdoc.fr/item/ZVMMF_2005_45_11_a14/