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Knight D. Pt. 2 . - 1988. - 17 p. : ill. - ([Reports] / American institute of aeronautics and astronautics(New York) ; n) Доп. точки доступа:
Экз-ры полностью e2e1ee411f406971a8df7ac228a9c9bf Копия: Нет сведений об экземплярах Держатели документа: Государственная публичная научно-техническая библиотека России : 123298, г. Москва, ул. 3-я Хорошевская, д. 17 (Шифр в БД-источнике (KATBW): R/2668/N/2)
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3-D shock wave-turbulent boundary layer interactions generated by a single fin / D. D. Knight, C. C. Horstman, G. S. Settles, 1993. - 23 p. - Текст : непосредственный. [Reports] / Amer.inst.of aeronautics and astronautics. N 89-0082 : experimental study of shock wave/vortex interaction : Rep. presented at 27th Aerospace sciences meet., Jan.9-12, 1989, Reno(Nv) / O.M.Metwally,G.S.Settles,C.C.Horstman, 1989. - 12 p. - Текст : непосредственный. [Reports] / Amer.inst.of aeronautics and astronautics. N 89-1852 : Computation of sharp fin and swept compression corner shock/turbulent boundary layer interactions : Rep.presented at AIAA 20th fluid dynamics, plasma dynamics and lasers conf.,Buffalo(NY), Jun.12-14,1989 / Y.Zang,D.D.Knight, 1989. - 12 p. - Текст : непосредственный. Knight D. Supersonic turbulent flow past a 3-D swept compression corner at mach 3 : Papers presented at AIAA 26th aerospace sci.meet., Jan. 11-14, 1988, Reno(Nv). Pt. 2, 1988. - 17 p. - Текст : непосредственный. Лицевая сторона карточки Обратная сторона карточки
Лицевая сторона карточки Обратная сторона карточки
Лицевая сторона карточки Обратная сторона карточки
Rhode D. A new efficient model for the computation of flow over shear layer driven cavities : Per.presented at AIAA/ASME/SAE/ASEE 25th joint propulsion conf., Monterey(Ca), Jul.10-12, 1989. Pt. 1 : Model development, 1989. - 7 p. - Текст : непосредственный. Rhode D. A new efficient model for the computation of flow over shear layer driven cavities : Per.presented at AIAA/ASME/SAE/ASEE 25th joint propulsion conf., Monterey(Ca), Jul.10-12, 1989. Pt. 2 : Assessment for labyrinth seal leakage, 1989. - 7 p. - Текст : непосредственный. Lee H. Effects of a melt-layer on the L*-instability in solid-propellant rockets : Rep.presented at 27th aerospace sciences meeting,Jan.9-12,1989/Reno(Nv) . Pt. I : Linear study, 1989. - 9 p. . - Текст : непосредственный. A study of three-dimensional natural convection in high pressure Mercury lamps : Paper presented 24th thermophysics conf., Buffalo(NY), June 12-14, 1989 / Chang P.,Dakin J.,Lighting G.E.,Shyy W. Pt. 1 : Parametric variations with horizontal mounting, 1989. - Pag.var. - Текст : непосредственный. Ruiz F. The regenerative internal combustion engine. Pt. 1 : Theory, 1988. - 8 p. - Текст : непосредственный. Investigation of unsteady flow through a transonic turbine stage : Rep. presented at the AIAA/SAE/ASME/ASEE 26th joint propulsion conf., July 16-18, 1990, Orlando(Fl) / Dunn M.G.,Bennett W.A.,Delaney R.A.,Rao K.V. Pt. 1 / K.V.Rao, R.A.Delaney, 1990. - 9 p. - Текст : непосредственный. Furlani T.R. A comparison of parallel algorithms for the direct simulation Monte Carlo method. Pt. 2 : Application to exhaust plume flowfields, 1989. - 22 p. - Текст : непосредственный. Liu Y. Equilibrium gas flow computations : Rep.presented at the AIAA 24th thermophysics conf.Buffalo(NY),June 12-14,1989. Pt. 1 : Accurate and efficient calculation of equilibrium gas properties, 1989. - 40 p. - Текст : непосредственный. Laminar boundary layer stability experiments on a cone at Mach 8 : Rep.presented at the AIAA 16th fluid and plasma dynamics conf.,July 12-14,1983,Danvers(Ma). Pt. 5 : Tests with a cooled model, 1989. - 30 p. - Текст : непосредственный. Jong F.de A combined eulerian-lagrangian two-phase flow analysis of SSME HPOTP nozzle plug trajectories : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf.,Monterey(Ca)/July 10-12,1989. Pt. 1 : Methodology, 1989. - 11 p. - Текст : непосредственный. Williams M. The multi-zone calculation of turbomachinery flows : Papers presented at AIAA/ASME/SAE/ASEE 24th joint propulsion conf., July 11-13, 1988, Boston(Ma). Pt. 2 : multizone calculation of the turbulent, two-specie flow through the SSME HPFTP first and second stage cavities, 1988. - 10 p. - Текст : непосредственный. Knight D. Supersonic turbulent flow past a 3-D swept compression corner at mach 3 : Papers presented at AIAA 26th aerospace sci.meet., Jan. 11-14, 1988, Reno(Nv). Pt. 2, 1988. - 17 p. - Текст : непосредственный. Заказать
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