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The optimized three-point fifth-order accurate generalized compact scheme
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2003, 21(4): 383-390.
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Experimental study on reducing large Bluff-based vehicles' drag by using guide vances (I)
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2003, 21(4): 391-398.
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Implementation of DWENO schemes and its application
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2003, 21(4): 399-407.
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The numerical simulation analysis of nappe-wind generated by flood discharge
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2003, 21(4): 408-416.
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Research of optimized design of three-dimensional contraction
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2003, 21(4): 417-423.
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Numerical simulation of periodically deforming circular cylinder
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2003, 21(4): 424-431.
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A study of gas dynamic gain performance of lateral jets
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2003, 21(4): 432-438.
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The optimization design of a simplified adaptive wing's aerodynamic shape
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2003, 21(4): 439-445.
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Nonlinear aerodynamic resilience and aerocraft dynamic stability
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2003, 21(4): 446-448.
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Numerical simulation of 2D multi-bodies with moving boundaries
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2003, 21(4): 449-453.
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Drag prediction of DLR-F4 from AIAA drag prediction workshop
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2003, 21(4): 454-458.
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A numerical method to calculate unsteady flow with Euler equations
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2003, 21(4): 459-463.
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Numerical simulation of supersonic lateral jet interactions for an axisymmetric body in supersonic flow
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2003, 21(4): 464-469.
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Investigation of transition effect on the pressure distribution of supercritical wing
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2003, 21(4): 470-475.
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The hypersonic chemical reaction flow of flat-nosed cylinder with hybrid DSMC/EPSM method
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2003, 21(4): 476-481.
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Numerical analysis of aerodynamics for missile with control-flaps
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2003, 21(4): 482-488.
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The 2002 annual report of research and development of aerodynamics in China
2003, 21(4): 489-500.
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