2002 No. 2

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Numerical analysis for correlation of standard model testing in high enthalpy facility and flight test
2002, 16(2): 1-8,20. doi: 10.3969/j.issn.1672-9897.2002.02.001
Abstract(90) PDF(3)
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Three-dimensional parallel simulation of the flow-field of a scramjet combustor and comparisons with experiments
2002, 16(2): 9-15. doi: 10.3969/j.issn.1672-9897.2002.02.002
Abstract(89) PDF(6)
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On the correlation of force test results of a tactical missile calibration model in five different wind tunnels
2002, 16(2): 16-20. doi: 10.3969/j.issn.1672-9897.2002.02.003
Abstract(144) PDF(6)
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Study on flow patterns over spur-dikes
2002, 16(2): 21-24,83. doi: 10.3969/j.issn.1672-9897.2002.02.004
Abstract(79) PDF(2)
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An investigation of increasing lift on large transport by using Gurney flap positioned at the trailing-edge
2002, 16(2): 25-29. doi: 10.3969/j.issn.1672-9897.2002.02.005
Abstract(129) PDF(4)
Abstract:
Effect of Gurney flaps on aerodynamical characters of single airfoil
2002, 16(2): 30-35. doi: 10.3969/j.issn.1672-9897.2002.02.006
Abstract(92) PDF(3)
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A direct experimental simulation of side-jet steering
2002, 16(2): 36-41. doi: 10.3969/j.issn.1672-9897.2002.02.007
Abstract(88) PDF(4)
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Experimental investigation on cavitation noise of an axisymmetric body
2002, 16(2): 42-46. doi: 10.3969/j.issn.1672-9897.2002.02.008
Abstract(122) PDF(3)
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Numerical Simulation of flame deformation induced by obstacle
2002, 16(2): 47-51. doi: 10.3969/j.issn.1672-9897.2002.02.009
Abstract(84) PDF(2)
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Effect of the apex flap on the leading edge vortex breakdown over a 70° delta wing
2002, 16(2): 52-56. doi: 10.3969/j.issn.1672-9897.2002.02.010
Abstract(95) PDF(3)
Abstract:
The design techniques of hypersonic Teflon cone and sabot for hypervelocity ballistic range tests
2002, 16(2): 57-62. doi: 10.3969/j.issn.1672-9897.2002.02.011
Abstract(139) PDF(4)
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Boundary layer simulation in the first test section of 8m×6m wind tunnel
2002, 16(2): 63-66. doi: 10.3969/j.issn.1672-9897.2002.02.012
Abstract(109) PDF(8)
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The location of boundary-layer transition detected by pressure fluctuation measurements
2002, 16(2): 67-71. doi: 10.3969/j.issn.1672-9897.2002.02.013
Abstract(112) PDF(9)
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The measurement on the turbulence jet with 3D LDV system
2002, 16(2): 72-77. doi: 10.3969/j.issn.1672-9897.2002.02.014
Abstract(126) PDF(7)
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Particle recognition of PTV measurement in gas-particle two-phase flow using fuzzy logic method
2002, 16(2): 78-83. doi: 10.3969/j.issn.1672-9897.2002.02.015
Abstract(100) PDF(2)
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Development and application of advance air source system for wind tunnel
2002, 16(2): 84-87. doi: 10.3969/j.issn.1672-9897.2002.02.016
Abstract(92) PDF(5)
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The survey of the inertia moment in free flight models
2002, 16(2): 88-91. doi: 10.3969/j.issn.1672-9897.2002.02.017
Abstract(100) PDF(3)
Abstract:
Test technique and application of large-scale pressure measurement in the 2.4m×2.4m transonic wind tunnel
2002, 16(2): 92-96. doi: 10.3969/j.issn.1672-9897.2002.02.018
Abstract(115) PDF(8)
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