Geodesic
"USSAERO" program modifications for asymmetric flow analysis
Theoretical and applied mechanics, Tome 16 (1990) no. 1, p. 65 Cet article a éte moissonné depuis la source eLibrary of Mathematical Institute of the Serbian Academy of Sciences and Arts

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The paper proposes an algorithm for the numerical analysis of the flow around a complex configuration in three-dimensional asymmetric flight. With the help of the modification and addition of the "USSAERO" program, it is possible to calculate the aerodynamic load of the aircraft under conditions of slip, roll and deflection of the command mechanization. The derived analysis applies only in the case of planar boundary conditions. 
@article{TAM_1990_16_1_a7,
     author = {Nikola Mladenovi\'c},
     title = {"USSAERO" program modifications for asymmetric flow analysis},
     journal = {Theoretical and applied mechanics},
     pages = {65 },
     year = {1990},
     volume = {16},
     number = {1},
     language = {en},
     url = {http://geodesic.mathdoc.fr/item/TAM_1990_16_1_a7/}
}
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Nikola Mladenović. "USSAERO" program modifications for asymmetric flow analysis. Theoretical and applied mechanics, Tome 16 (1990) no. 1, p. 65 . http://geodesic.mathdoc.fr/item/TAM_1990_16_1_a7/