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Requirement of fighter development to stealth and aerdoynamic technology
2002, 16(1): 1-7，26. DOI: 10.3969/j.issn.1672-9897.2002.01.001
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The calculations of aerodynamic heating and viscous friction forces on the surface of hypersonic flight vehicle
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2002, 16(1): 8-20. DOI: 10.3969/j.issn.1672-9897.2002.01.002
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Experimental studies of the characteristics of the flow about a grid fin
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2002, 16(1): 21-26. DOI: 10.3969/j.issn.1672-9897.2002.01.003
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Analysis of the dispenser aerodynamic characteristics
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2002, 16(1): 27-32. DOI: 10.3969/j.issn.1672-9897.2002.01.004
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Measurement on constitutive equation of granular materials
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2002, 16(1): 33-35，60. DOI: 10.3969/j.issn.1672-9897.2002.01.005
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Wind tunnel research on wind loading on a stage with the shape of elliptical sphere
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2002, 16(1): 36-42. DOI: 10.3969/j.issn.1672-9897.2002.01.006
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The application of chimera grid technique and the viscous flow numerical simulation to wind tunnel wall interference study
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2002, 16(1): 43-49. DOI: 10.3969/j.issn.1672-9897.2002.01.007
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An experimental investigation on helicopter scissors rotors in hover
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2002, 16(1): 50-55. DOI: 10.3969/j.issn.1672-9897.2002.01.008
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A new type of movable inclined tail gate for improving flume flow pattern
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2002, 16(1): 56-60. DOI: 10.3969/j.issn.1672-9897.2002.01.009
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The aerodynamic design of supersonic quiet wind tunnel
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2002, 16(1): 61-66. DOI: 10.3969/j.issn.1672-9897.2002.01.010
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Numerical simulation of hypersonic flowfield around sphere model and experimental verification
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2002, 16(1): 67-73，79. DOI: 10.3969/j.issn.1672-9897.2002.01.011
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The measurement of infrared radiation for ballistic range
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2002, 16(1): 74-79. DOI: 10.3969/j.issn.1672-9897.2002.01.012
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Colored CFI-interferometry in experimental interferogram processing for hypersonic blunted cone flow in ballistic range
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2002, 16(1): 80-86，93. DOI: 10.3969/j.issn.1672-9897.2002.01.013
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Development of the six-component force-measuring balance for thrust-vectoring nozzle testing
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2002, 16(1): 87-93. DOI: 10.3969/j.issn.1672-9897.2002.01.014
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The development of the wind tunnel balance measuring for tiny roll moment with gas bearing
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2002, 16(1): 94-98. DOI: 10.3969/j.issn.1672-9897.2002.01.015
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On the supersonic impinging jet by Laser Doppler Velocimetry
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2002, 16(1): 99-103. DOI: 10.3969/j.issn.1672-9897.2002.01.016
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Calculation of pressure distributions of low aspect ratio missile wings at supersonic speeds and high angles of attack
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2002, 16(1): 104-107. DOI: 10.3969/j.issn.1672-9897.2002.01.017
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