Display Method:
Analysis of an aeroelastic system with bilinear stiffness using the cell mapping method
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2002, 20(2): 123-132.
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An implicit gridless method and its applications
2002, 20(2): 133-140.
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Airfoil aerodynamic design and optimization based on Navier-Stokes equations
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2002, 20(2): 141-149.
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The characteristics of flow structure and heat transfer in circular pipe rotating about an arbitrary axis
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2002, 20(2): 150-157.
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The analysis of gyroidal reentry trajectory for maneuver missile with bend-nose
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2002, 20(2): 158-164.
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Numerical simulation of three-dimensional turbulent boundary layer with nonlinear eddy-viscosity model
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2002, 20(2): 165-173.
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The analyses of aerodynamic characters of multi-element airfoil with Gurney flap
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2002, 20(2): 174-178.
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Applied study of method for multi-block patched mesh
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2002, 20(2): 179-183.
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Numerical simulation of hypersonic ionized flows
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2002, 20(2): 184-191.
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Analysis of global stability and nonlinear control for a fighter configuration
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2002, 20(2): 192-197.
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Effects of near-wall turbulence model on numerical simulation of turbulent separated flows
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2002, 20(2): 198-205.
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The study of hybrid DSMC/EPSM method of supersonic flat-nosed cylinder
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2002, 20(2): 206-210.
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Investigation of Rayleigh-Benard instability in rarefied gas by DSMC method
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2002, 20(2): 211-216.
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The simulation of fluid control by microactuators
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2002, 20(2): 217-221.
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Aerodynamic analysis of a Variable-bend-tail vehicle
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2002, 20(2): 222-226.
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Three-dimensional numerical simulation of the airflow in an apartment unit
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2002, 20(2): 227-232.
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The wind tunnel test study on wind load shape coefficient of aqueduct body structure for U shape
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2002, 20(2): 233-238,.
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Numerical studies of non-equilibrium flow-fields over a capsule-type hypersonic reentry vehicle
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2002, 20(2): 239-245.
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