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Display Method:
Aerodynamic parameter identification of rapid self-rotating flight vehicle
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2004, 22(1): 1-6.
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Influence of nose bluntness on behaviors of multi-asymmetric vortices flow over slender body
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2004, 22(1): 7-13.
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Estimation the turbulent dissipation rate in a horizontal rectangular duct by large eddy PIV method
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2004, 22(1): 14-19.
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Simulation on double two-phase fluid heat exchanger
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2004, 22(1): 20-23.
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The prediction of thermal protection performance for coating material
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2004, 22(1): 24-28.
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Study of separated flow in a diffuser using linear and nonlinear eddy-viscosity turbulence models
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2004, 22(1): 29-35.
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Wind tunnel experimental research on aerodynamic improvement of UAV
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2004, 22(1): 36-40.
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Wind load on cantilevered structures of long span roofs
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2004, 22(1): 41-46.
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Aeroacoustic noise prediction of helicopter rotor in forward flight using Kirchhoff method
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2004, 22(1): 47-51.
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Numerical simulation and mechanism study of the interaction of adjacent synthetic jet actuators
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2004, 22(1): 52-59.
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Numerical analysis of flow in a lobed exhaust-ejector with a double-wall diffuser
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2004, 22(1): 60-63.
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Computational simulation of three dimensional unsteady flow field induced by a body overtaking a shock wave
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2004, 22(1): 64-68.
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The experimental study of convection characteristics of the multi-scale eddy structure in turbulent jet flow
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2004, 22(1): 69-72.
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Numerical simulation of viscous supersonic flows by finite spectral method
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2004, 22(1): 73-79.
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Sectional topological structure research of 3D complex figuration at different angles of attack
2004, 22(1): 80-83.
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Numerical study of the far-filed intensity distribution of laser beam disturbed by shock wave
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2004, 22(1): 84-87.
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Using sensitivity method to reduce the chemical reaction kinetics model
2004, 22(1): 88-92.
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Side-wall boundary layer removal at airfoil test based on Navier-Stokes equations
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2004, 22(1): 93-96.
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Application of the free molecule point source model to the plume field with nonuniform outlet conditions
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2004, 22(1): 97-100.
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A study on vortex shedding frequency of blade profile and cylinder in cascade tunnel
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2004, 22(1): 101-108.
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Hyperbolic grid generation using upwind scheme
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2004, 22(1): 109-113.
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Simulation of the release of store based on the moving chimera grid technique
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2004, 22(1): 114-117.
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