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Study on gas kinetic unified algorithm for flows from rarefied transition to continuum
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2003, 21(3): 255-266.
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Numerical study on synthetic flow field of adjacent microjet actuators
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2003, 21(3): 267-274.
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Investigation of integrated multi-disciplinary and multi-objective optimization of the aircraft configuration design method
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2003, 21(3): 275-281.
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Experiment study of hypersonic six-component force measurement for re-entry module in shock tunnel
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2003, 21(3): 282-287.
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Computation of flows around projectile bodies with base jet using finite-volume method of Navier-Stokes equations
2003, 21(3): 288-294.
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The numberial reseach of wake impacting effect in 2D subsonic compressor cascad
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2003, 21(3): 295-300.
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Apply the CE/SE method to the simulation of unsteady detonation
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2003, 21(3): 301-310.
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Numerical analysis of indoor air distribution and indoor air quality on three ventilation patterns
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2003, 21(3): 311-319.
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Research advances on a close-coupled canard wing configuration
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2003, 21(3): 320-329.
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Quasi-steady-state three shock wave structure
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2003, 21(3): 330-335.
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Characteristic analysis of the upwind scheme
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2003, 21(3): 336-341.
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Second-order perturbational finite difference schemes for hyperbolic conservation equation
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2003, 21(3): 342-350.
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Numerical simulation of turbulence flows about a slender pointed body at high angle of attack
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2003, 21(3): 351-355.
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Numerical simulation of airframe/inlet viscous flow
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2003, 21(3): 356-361.
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General summarization of aerodynamic characteristics of european crew transfer vehicle CTV
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2003, 21(3): 362-367.
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A fractional step method for the time dependent incompressible Navier-Stokes/Euler coupled equations
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2003, 21(3): 368-375.
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Numerical study on tunnel-hood when high-speed train passing a tunnel
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2003, 21(3): 376-381.
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