Geodesic
Supersonic flow around a body of small elongation
Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 5 (2009), pp. 69-71 Cet article a éte moissonné depuis la source Math-Net.Ru

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The results of experimental studies conducted in an aerodynamic tube at the Mach number $\mathrm{M}=1{,}78$ for a model of a blunt-shaped body of small elongation are given. The effect of the attack angle on the coefficients of drag and lifts, the static stability, and the pressure center position is discussed. 
@article{VMUMM_2009_5_a16,
     author = {S. V. Guvernyuk and A. F. Zubkov and K. M. Pichkhadze and V. S. Finchenko and A. I. Shvets},
     title = {Supersonic flow around a body of small elongation},
     journal = {Vestnik Moskovskogo universiteta. Matematika, mehanika},
     pages = {69--71},
     year = {2009},
     number = {5},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMUMM_2009_5_a16/}
}
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S. V. Guvernyuk; A. F. Zubkov; K. M. Pichkhadze; V. S. Finchenko; A. I. Shvets. Supersonic flow around a body of small elongation. Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 5 (2009), pp. 69-71. http://geodesic.mathdoc.fr/item/VMUMM_2009_5_a16/