Journal of Nanjing University of Aeronautics & Astronautics, Volume 37, Number 6, December 2005.
(30/05/2013)
Partial Contents: Numerical Simulation of Rotor Flowfield Based on Embedded Grids and Incorporated Wake Effects; Aerodynamical Characteristics Analysis of Ducted Fan; Performance Effects of Geometry Parameters on Hypersonic Inlet; Cylinder Type Non-Contact Ultrasonic Motor; Monte Carlo Simulation on Low-Energy Electrons Scattering in Ni. NiTi and Ti Bulks; Numerical Simulation on Thermally Driven Heat Transfer in Enclosure Filled with Porous Medium; Numerical Study of Cold Flow Field in Gas Turbine Combustor; Stability Characteristic of Double-Intet Fulse Tube Cooler; Aerodynamic Design Optimization of Turbine Blade Based on Multidiscipline; Stability Analysis of Nonparallel Boundary Layers on Wings; Virtual Reality and Simulation of Material...
Tác giả: Dewang, L. |
Số trang: 162 |
Lĩnh vực: Vũ trụ |
Năm XB: 2005 |
Loại tài liệu: Khác
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Partial Contents: Numerical Simulation of Rotor Flowfield Based on Embedded Grids and Incorporated Wake Effects; Aerodynamical Characteristics Analysis of Ducted Fan; Performance Effects of Geometry Parameters on Hypersonic Inlet; Cylinder Type Non-Contact Ultrasonic Motor; Monte Carlo Simulation on Low-Energy Electrons Scattering in Ni. NiTi and Ti Bulks; Numerical Simulation on Thermally Driven Heat Transfer in Enclosure Filled with Porous Medium; Numerical Study of Cold Flow Field in Gas Turbine Combustor; Stability Characteristic of Double-Intet Fulse Tube Cooler; Aerodynamic Design Optimization of Turbine Blade Based on Multidiscipline; Stability Analysis of Nonparallel Boundary Layers on Wings; Virtual Reality and Simulation of Material Deformation.
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