2002 No. 3

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Investigation on wing rock characteristics for a fighter configuration
2002, 16(3): 1-7. doi: 10.3969/j.issn.1672-9897.2002.03.001
Abstract(83) PDF(2)
Abstract:
The investigation of engine simulation test with ejector in high speed wind tunnel
2002, 16(3): 8-13. doi: 10.3969/j.issn.1672-9897.2002.03.002
Abstract(89) PDF(4)
Abstract:
Correlation study on data of force-measuring test in hypersonic wind tunnel
2002, 16(3): 14-18,25. doi: 10.3969/j.issn.1672-9897.2002.03.003
Abstract(123) PDF(6)
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Investigation on the wind resistant properties of Nancha bridge
2002, 16(3): 19-25. doi: 10.3969/j.issn.1672-9897.2002.03.004
Abstract(89) PDF(2)
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Water tunnel flow visualization study of a canard-configuration aircraft model
2002, 16(3): 26-31. doi: 10.3969/j.issn.1672-9897.2002.03.005
Abstract(85) PDF(3)
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Field measurements of strong wind characteristics near ground in Pudong district
2002, 16(3): 32-39. doi: 10.3969/j.issn.1672-9897.2002.03.006
Abstract(95) PDF(9)
Abstract:
The research of ejection seat test
2002, 16(3): 40-45. doi: 10.3969/j.issn.1672-9897.2002.03.007
Abstract(68) PDF(3)
Abstract:
Development of balance used in unmanned craft propeller testing
2002, 16(3): 46-50. doi: 10.3969/j.issn.1672-9897.2002.03.008
Abstract(106) PDF(4)
Abstract:
Simulation technique for improving data precision and accuracy of maximum hinge moment test
2002, 16(3): 51-56. doi: 10.3969/j.issn.1672-9897.2002.03.009
Abstract(136) PDF(2)
Abstract:
Rebuilding control and measurement system of CG-01 wind tunnel
2002, 16(3): 57-62. doi: 10.3969/j.issn.1672-9897.2002.03.010
Abstract(117) PDF(6)
Abstract:
Experimental technique for rolling aerodynamic of slight asymmetric re-entry body
2002, 16(3): 63-67,72. doi: 10.3969/j.issn.1672-9897.2002.03.011
Abstract(128) PDF(4)
Abstract:
The application of intelligent control to the synchronization control systems of 2.4m wind tunnel
2002, 16(3): 68-72. doi: 10.3969/j.issn.1672-9897.2002.03.012
Abstract(109) PDF(3)
Abstract:
Active control isolation simulink research for a class of nonlinear chaotic vibration systems in equipments
2002, 16(3): 73-79. doi: 10.3969/j.issn.1672-9897.2002.03.013
Abstract(99) PDF(3)
Abstract:
Analysis of problem on measuring value correction formula of differential pressure type gas flow-metering
2002, 16(3): 80-85. doi: 10.3969/j.issn.1672-9897.2002.03.014
Abstract(126) PDF(6)
Abstract:
Method study on aerodynamic engineering approximation of missiles with non-circular shape cross sections
2002, 16(3): 86-90. doi: 10.3969/j.issn.1672-9897.2002.03.015
Abstract(90) PDF(2)
Abstract:
Assessments of measurement uncertainty of wind tunnel test based on symbolic math
2002, 16(3): 91-95. doi: 10.3969/j.issn.1672-9897.2002.03.016
Abstract(86) PDF(4)
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