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Technical ways to solve high speed key aerodynamic problems of large air transporters
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2004, 18(2): 1-5. DOI: 10.3969/j.issn.1672-9897.2004.02.001
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A base code for aircraft synthetic design and evaluation
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2004, 18(2): 6-10. DOI: 10.3969/j.issn.1672-9897.2004.02.002
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A summary of wind tunnel test techniques for high-altitude long-endurance UAV
2004, 18(2): 11-16. DOI: 10.3969/j.issn.1672-9897.2004.02.003
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Pressure transient analysis and control of water hammer device
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2004, 18(2): 17-19,24. DOI: 10.3969/j.issn.1672-9897.2004.02.004
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Test technique of hinge-moment in 8m × 6m wind tunnel
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2004, 18(2): 20-24. DOI: 10.3969/j.issn.1672-9897.2004.02.005
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Study on flow characteristics over air refueling tubes
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2004, 18(2): 25-27,54. DOI: 10.3969/j.issn.1672-9897.2004.02.006
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The design and calibration of ejected engine simulator
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2004, 18(2): 28-31. DOI: 10.3969/j.issn.1672-9897.2004.02.007
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Discussion on the simulation of atmospheric boundary layer with spires and roughness elements in wind tunnels
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2004, 18(2): 32-37. DOI: 10.3969/j.issn.1672-9897.2004.02.008
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Correlation investigation of unsteady aerodynamics of dynamic delta wings and pressure distribution
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2004, 18(2): 38-42. DOI: 10.3969/j.issn.1672-9897.2004.02.009
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The wind tunnel experiment techniques of backward dispersion of turning shrapnel
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2004, 18(2): 43-46. DOI: 10.3969/j.issn.1672-9897.2004.02.010
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The optimization study of optical performance of shear layer in free-vortex ADW
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2004, 18(2): 47-49. DOI: 10.3969/j.issn.1672-9897.2004.02.011
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A new approach for experimental model to realize the sinusoidal motions of heaving and pitching in phase
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2004, 18(2): 50-54. DOI: 10.3969/j.issn.1672-9897.2004.02.012
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The experiment exploration of catalyst effects on aerodynamic heat in real gas effects
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2004, 18(2): 55-58,64. DOI: 10.3969/j.issn.1672-9897.2004.02.013
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An experimental study of turbulent boundary layer over the grooved-surface
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2004, 18(2): 59-64. DOI: 10.3969/j.issn.1672-9897.2004.02.014
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The characteristics of nose vortices and Karman vortices in the flow over slender body at high angles of attack
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2004, 18(2): 65-70. DOI: 10.3969/j.issn.1672-9897.2004.02.015
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The visualization of vortex field of unsteady motion for 2-D foil--heaving motion
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2004, 18(2): 71-76. DOI: 10.3969/j.issn.1672-9897.2004.02.016
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Development on the half model balance in the 2.4 m × 2.4 m transonic wind tunnel
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2004, 18(2): 77-81,85. DOI: 10.3969/j.issn.1672-9897.2004.02.017
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Fluid dynamic characteristic measurement of high pressure nozzle used in extinguishing system
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2004, 18(2): 82-85. DOI: 10.3969/j.issn.1672-9897.2004.02.018
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Experimental measurements of the turbulence characteristics under sheared air-water interfaces
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2004, 18(2): 86-90. DOI: 10.3969/j.issn.1672-9897.2004.02.019
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Section model wind tunnel test for steady aerodynamic force of line-like multi-body system
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2004, 18(2): 91-94. DOI: 10.3969/j.issn.1672-9897.2004.02.020
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An algorithm for balance formula
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2004, 18(2): 95-97,101. DOI: 10.3969/j.issn.1672-9897.2004.02.021
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The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet
2004, 18(2): 98-101. DOI: 10.3969/j.issn.1672-9897.2004.02.022
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