Geodesic
Geometric modeling of complex configurations in aerodynamic problems
Numerical methods and programming, Tome 2 (2001) no. 1, pp. 112-122.

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An analytical method for the construction of a geometric model that can be used for numerical studies of spatial supersonic flows over complex aerodynamic configurations is proposed. Some analytical relations for constructing the complex geometry of bodies and a building algorithm for isolated variable sweepback wings with parabolic profiles and flat midsurface are given. The problem of constructing the geometry of composite configurations of higher levels (such as a “body+wing” combination ) is considered; an algorithm for the realization of joining the components of this geometry is described. The problem of spatial wing flow for the supersonic civil transport TU-144 is analyzed numerically for Mach number $M=2.27$ and angles of attack range from 1.3 to 8.3 degrees. Our numerical results are compared with data of physical experiments.
Keywords: geometric models, numerical simulation, spatial flows, wing, wing geometry. 
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     author = {V. F. Volkov},
     title = {Geometric modeling of complex configurations in aerodynamic problems},
     journal = {Numerical methods and programming},
     pages = {112--122},
     publisher = {mathdoc},
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     number = {1},
     year = {2001},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMP_2001_2_1_a7/}
}
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V. F. Volkov. Geometric modeling of complex configurations in aerodynamic problems. Numerical methods and programming, Tome 2 (2001) no. 1, pp. 112-122. http://geodesic.mathdoc.fr/item/VMP_2001_2_1_a7/