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Study on convergence to steady state of the time splitting method for conservation laws with source terms
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2004, 22(4): 377-383,.
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Investigation on unsteady wind-tunnel wall interference
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2004, 22(4): 384-388.
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Aerodynamically design of a supersonic nozzle used in z-pinch gas puffs by numerical simulation
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2004, 22(4): 389-394,.
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Numerical Simulation of Supersonic Flow in Combustor with Dual-Cavity
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2004, 22(4): 395-398.
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Numerical study of interactive flowfields with lateral jet
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2004, 22(4): 399-403.
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Improvement of AUSM+ scheme
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2004, 22(4): 404-409.
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Design of airfoil with high ratio of lift over drag
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2004, 22(4): 410-415.
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An investigation for the evolvement of disturbances in 3-D compressible mixing layer
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2004, 22(4): 416-421.
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Mechanisms of breakup and atomization of a viscous liquid jet in a viscous gas
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2004, 22(4): 422-426.
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Adaptive cartesian grid method in numerical simulation of flow field about civil-plane high-lift system
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2004, 22(4): 427-431,.
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The development of an unsteady numerical methods and its application on dynamic vehicle flows
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2004, 22(4): 432-437.
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A study of inverse problem for dam seepage flow
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2004, 22(4): 438-442.
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Inverse design of airfoil based on variable-domain variational FEM
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2004, 22(4): 443-446,.
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Direct simulation of Monte Carlo(DSMC) of rarefied gas flow in Crookes radiometer
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2004, 22(4): 447-451.
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The measurements of aerodynamic force property and geometric, physical parameter of javelin
2004, 22(4): 452-456.
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Simplified buffeting analysis in time domain on the basis of ANSYS for cable-stayed bridge
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2004, 22(4): 457-460.
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A study of the boundary condition in the DNS of the supersonic boundary layer flow
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2004, 22(4): 461-465.
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The effects of unsteady free stream on aerodynamics of an aircraft model
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2004, 22(4): 466-469.
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Effects of imbalance of LU-SGS implicit algorithm using unstructured grid
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2004, 22(4): 470-474.
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Numerical simulations of pre-detonation ignition of pulse detonation engines
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2004, 22(4): 475-480,.
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Grid influence in computing the high-alpha aerodynamics of delta wings
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2004, 22(4): 481-485.
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Asymmetric vortex structure of slender revolution at high angles of attack
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2004, 22(4): 486-489,.
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Computation of glaze ice accretion on airfoil
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2004, 22(4): 490-493.
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The character research of aerodynamic heating on lifting body model using infrared thermographic technique
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2004, 22(4): 494-498,.
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Adaptation of QUICK schemes under uneven grids to the calculations of strongly separated turbulent flow
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2004, 22(4): 499-503.
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