Электронный каталог

    страница из
    всего найдено записей: 6,
      отображать

    Лицевая сторона карточкиОбратная сторона карточки

    Лицевая сторона карточкиОбратная сторона карточки

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-1849 : Measurements of swept shock wave/turbulent boundary-layer interactions by holographic interferometry : Rep. presented at AIAA 20th fluid dynamics, plasma dynamics a. lasers conf., Buffalo(NY), June 12-14, 1989 / J.Hsu,G.Settles, 1989. - 10 p. - Текст : непосредственный.

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-1850 : Inception length to a fully-developed fin-generated shock wave boundary-layer interaction : Rep. presented at AIAA 20th fluid dynamics, plasma dynamics a. lasers conf., Buffalo(NY), June 12-14, 1989 / F.Lu,G.Settles, 1989. - 11 p. - Текст : непосредственный.

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-2456 : experimental study of the effect of streamwise vorticity on supersonic mixing enhancement : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf., Monterey(Ca), July 10-12, 1989 / J.Naughton,L.Cattafesta,G.Settles, 1989. - 22 p. - Текст : непосредственный.

    Alvi F. Structure of swept shock wave/boundary-layer interactions using conical shadowgraphy : Paper presented at AIAA 21st fluid dynamics,plasma dynamics and lasers conf.,June 18-20,1990,Seattle(Wa)8-9 / F.Alvi,G.Settles, 1990. - 10 p. - Текст : непосредственный.