Вход
Электронный каталог
[Reports] / Amer.inst.of aeronautics and astronautics. N 89-1654 : control volume based finite element formulation of the compressible flow equations with application to the shock tube problem : Rep. presented at the AIAA 24th thermophysics conf., Buffalo(NY)/June 12-14,1989 / G.E.Schneider,E.Kochavi, 1989. - 9 p. - Текст : непосредственный.