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Simulation of mixing-layer gas-particle flows using a two-fluid particle-wall collision model
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2004, 22(3): 249-254.
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Numerical determination of trim angle of attack for reentry vehicles using dynamic unstructured grids
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2004, 22(3): 255-258.
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Calculation of hybrid problems for aerodynamic design of cascade using combined mesh
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2004, 22(3): 259-264.
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Analysis and comparison of multi-conservation difference schemes
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2004, 22(3): 265-268.
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Study of higher order accuracy algorithm of capturing discontinuity
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2004, 22(3): 269-273.
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Study to the combustion performance of a scramjet combustor with struts
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2004, 22(3): 274-278.
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Investigation on flow-field debugging for 2.4m transonic wind tunnel
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2004, 22(3): 279-282.
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An ALE method for vortex-induced vibrations of an elastic circular cylinder
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2004, 22(3): 283-288.
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Convergence performance of SIMPLE-like algorithm on unstructured grids
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2004, 22(3): 289-294.
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Unsteady characteristic research of lateral jet in hypersonic external flow
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2004, 22(3): 295-302.
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Numerical investigations of wake and force for flow past a sphere
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2004, 22(3): 303-308.
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Numerical simulation of lateral jet control of a hypersonic missile
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2004, 22(3): 309-312.
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Euler solutions of transonic flow for a helicopter rotor in hover using multigrid method
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2004, 22(3): 313-318.
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Numerical simulations of turbulent spots in channel flow
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2004, 22(3): 319-324.
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Wind tunnel test research for fluctuating pressure on large-span complex foof
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2004, 22(3): 325-331.
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The study of limit cycle flutter for airfoil with nonlinearity
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2004, 22(3): 332-336.
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The computation of a wing-body combination with aileron
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2004, 22(3): 337-341.
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An extension to Ludwieg's stability criterion for compressible swirling flow
2004, 22(3): 342-345.
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Model experiment and numeral simulation of the aerodynamics character of high-speed train entering tunnel
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2004, 22(3): 346-351.
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Investigation on computation method of LTE model parameter for high temperature gases and its application in the state diagnosis of non-equilibrium arcjet
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2004, 22(3): 352-356.
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A type of DRP finite difference schemes for aeroacoustic problems
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2004, 22(3): 357-360.
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Numerical investigation for six types of hypersonic turbulent shock-shock interaction
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2004, 22(3): 361-364.
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Simulating wind series with intermittency
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2004, 22(3): 365-370.
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Optimal integrated design of two-dimensional hypersonic vehicle's forebodies and inlets
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2004, 22(3): 371-375.
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