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Display Method:
Significance of diffusion-parabolized NS equations and its application to computational fluid dynamics
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2003, 21(1): 1-10.
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Subsonic and transonic wing inverse design using control theory
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2003, 21(1): 11-19.
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Investigation of characteristics of asymmetry flows and control of acoustic excitation on a slender revolutionary body at high angle of attack
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2003, 21(1): 20-28.
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An experimental study of flow patterns over the upswept after-body of a civil aircraft
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2003, 21(1): 29-37.
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Numerical analysis of interactive vortex-shedding from a pair of circular cylinders in a transverse arrangement by random vortex method
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2003, 21(1): 38-46.
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The numerical simulation of submution separation processes from dispenser
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2003, 21(1): 47-52.
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A new nonequilibrium numerical method and simulation of oscillating shock-induced combustion
2003, 21(1): 53-58.
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Numerical simulation of gaseous detonation with detailed chemical reaction model
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2003, 21(1): 59-66.
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Analysis of the flows and the drag about upswept afterbodies
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2003, 21(1): 67-74.
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The variation of the 3-dimensional structures of flow separation with Reynolds number for a prolate spheroid
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2003, 21(1): 75-81.
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Comparison of two difference schemes and two turbulence models in the numerical computations of an axisymmetric impinging jet flow
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2003, 21(1): 82-89.
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Application of embedding grid technology in numerical simulation about 3-D lift-enhancing device
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2003, 21(1): 90-97.
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Simulation of two-phase turbulent flow using a two-fluid model
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2003, 21(1): 98-103.
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Studying of multi-plume interference effects for attitude-control thruster with DSMC method
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2003, 21(1): 104-108.
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Joint grid system applied for the configuration of body-strake-wing
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2003, 21(1): 109-113.
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The experimental study for the sound radiation by the vibrational nozzle
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2003, 21(1): 114-119.
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The finite element equation solution method study based on EBE strategy for fluid field problem
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2003, 21(1): 120-127.
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