Geodesic
Some problems of the optimal aerodynamic design of bodies with minimal heat transfer
The Bulletin of Irkutsk State University. Series Mathematics, Tome 3 (2010) no. 3, pp. 41-50 Cet article a éte moissonné depuis la source Math-Net.Ru

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The spacecraft form is known to affect its aerodynamic and thermal characteristics strongly. This paper formulates and solves variational problems of finding optimal forms of flat and axisymmetric bodies from the standpoint of the minimum of the total heating along the flight trajectory. These body shapes allow the heat surface fluxes to be reduced by 20–50%.
Keywords: optimal aerodynamic design, variational problems, non-additive functional, heat transfer, computational methods. 
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M. A. Arguchintseva. Some problems of the optimal aerodynamic design of bodies with minimal heat transfer. The Bulletin of Irkutsk State University. Series Mathematics, Tome 3 (2010) no. 3, pp. 41-50. http://geodesic.mathdoc.fr/item/IIGUM_2010_3_3_a3/

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