ГПНТБ России - Полное описание

Государственная публичная
научно-техническая библиотека России

Основана в 1958 году

Полное описание

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[Reports] / Amer.inst.of aeronautics and astronautics. N 90-0243 : Derivation and testing of a new multi-scale k-e turbulence model : Rep.presented at the AIAA 28th aerospace sciences meet.Jan.8-11,1990/Reno(Nv) / S.H.Ko,D.L.Rhode, 1990. - 9 p. - Текст : непосредственный.

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[Reports] / Amer.inst.of aeronautics and astronautics. N 88-2884 : Numerical and experimental evaluation of a new low-leakage labyrinth seal : Rep.presented at AIAA/ASME/SAE/ASEE 24 joint propulsion conf.Jul.11-13, 1988, Boston(Ma) / D.L.Rhode,S.H.Ko,G.L.Morrison, 1988. - 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. 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.

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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.

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