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Display Method:
The perturbation solutions of the flow in a rotating curved annular pipe
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2003, 21(2): 129-136.
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Distributed evolutionary algorithms for inverse design problems of airfoil in aerodynamics
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2003, 21(2): 137-143.
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Investigation of numerical method for unstructured/hybrid grid
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2003, 21(2): 144-150.
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A study on flight performance of a Variable-Bend-Tail Vehicle
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2003, 21(2): 151-156.
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Study of crossflow topology of unsteady vortex motion over a delta wing
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2003, 21(2): 157-163.
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One-dimensional numerical computation for equation of state of gaseous methane under shock compression
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2003, 21(2): 164-172.
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Study of algorithm for multi-block patched mesh applied to hypersonic flow
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2003, 21(2): 173-181.
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Air-admission mechanism and low speed tunnel test of a submerged inlet with low RCS missile body
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2003, 21(2): 182-188.
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Numerical simulation of aerodynamic coefficients of the aircraft canopy
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2003, 21(2): 189-195.
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Application of genetic algorithms for aerodynamic parameter estimation
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2003, 21(2): 196-201.
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Applications of 3-D adaptive Cartesian grid algorithm based on the Euler equations
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2003, 21(2): 202-210.
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Vibrational spires method in wind tunnel simulation of atmospheric boundary layer
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2003, 21(2): 211-217.
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Double weighted essentially non-oscillatory shock-capturing schemes
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2003, 21(2): 218-225.
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Numerical simulation of Navier-Stokes equations for flowfields around the vehicles of complex configuration
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2003, 21(2): 226-230.
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Numerical study of supersonic turbulence flows on 2-D cavity
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2003, 21(2): 231-236.
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Research on the orientation of cylindrical particles in gas-solid two-phase pipe Flows
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2003, 21(2): 237-243.
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Numerical study on the external flow field of micro jet actuator
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2003, 21(2): 244-249.
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A study of lateral directional aerodynamic characteristics for combinations at high angle of attack
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2003, 21(2): 250-254.
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