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Progress in large eddy simulation of turbulent flows
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2004, 22(2): 121-129.
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Study of the dynamic stability of a pitching unfinned reentry capsule
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2004, 22(2): 130-134.
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Measurements of the flow field through windbreaks of different type with Particle Image Velocimetry(PIV)
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2004, 22(2): 135-140,.
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Supersonic jet screech suppression by a shield and it's effects on the flow
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2004, 22(2): 141-146.
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Study to the performance of the fuel diffusion in a scramjet combustion chamber with struts
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2004, 22(2): 147-150.
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Experiment research on the rotor autorotation state for a high-speed helicopter scheme
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2004, 22(2): 151-155.
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Numerical simulation of the rocket-exhaust impimgement flowfield in a helical tube launcher
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2004, 22(2): 156-159,.
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The research of computational method of aerodynamic load based on nmnerical simulation
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2004, 22(2): 160-164.
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Vortices structure and pressure fluctuation characteristics of the flow over slender body at high angles of attack
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2004, 22(2): 165-170.
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Aerodynamics prediction and configuration optimization for reentry vehicle with double-ellipse cross-section
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2004, 22(2): 171-174.
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A new method based on the dynamic evolution of airfoil
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2004, 22(2): 175-179.
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Research of aerodynamic optimization method based on dynamic boundary control
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2004, 22(2): 180-184.
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CFD-based numerical simulation of electromagnetic scattering
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2004, 22(2): 185-189.
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The aerodynamic characteristics of freewing
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2004, 22(2): 190-195.
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Ensemble-average three-dimensional velocity measurement in the tip region of axial rotor with tip clearance
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2004, 22(2): 196-200.
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Analyze around flow characteristics of tactical missile model at high angles of attack and high Mach numbers
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2004, 22(2): 201-205.
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Weighted compact high-order nonlinear scheme WCNS-E-5 applied to two dimensional flows
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2004, 22(2): 206-210.
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The study of heat transfer rate around complicated configurations in hypersonic flows using NND finite-element method
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2004, 22(2): 211-215.
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Spectral element method in polar coordinate for incompressible Navier-Stokes equations
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2004, 22(2): 216-219.
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Favorable influence of swept shock-boundary layer interactions
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2004, 22(2): 220-224.
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Experimental investigation of Xiao Shan International Trade Centre in wind tunnel
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2004, 22(2): 225-230.
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Dynamic hybrid grid generation for complex geometries
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2004, 22(2): 231-236.
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Experimental investigation on longitudinal aerodynamic characteristics of Canard-Forward-Swept wing configuration
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2004, 22(2): 237-240,.
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The numerical calculation research of two dimensional aileron by solving N-S equation
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2004, 22(2): 241-244.
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Research on the definition of pitching static margin for flight vehicle
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2004, 22(2): 245-248.
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