2004 No. 4

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New systems,concepts and techniques in the area of foreign wind tunnel test
2004, 18(4): 1-6. doi: 10.3969/j.issn.1672-9897.2004.04.001
Abstract(100) PDF(9)
Abstract:
A new technique of mixing augmentation for supersonic combustion flows
2004, 18(4): 7-10. doi: 10.3969/j.issn.1672-9897.2004.04.002
Abstract(103) PDF(3)
Abstract:
Effects of roll angle on side force distribution over slender bodies of revolution at high angle of attack
2004, 18(4): 11-14,19. doi: 10.3969/j.issn.1672-9897.2004.04.003
Abstract(104) PDF(3)
Abstract:
Experimental study on explosive dispersion and cloud formation of liquid fuel
2004, 18(4): 15-19. doi: 10.3969/j.issn.1672-9897.2004.04.004
Abstract(82) PDF(7)
Abstract:
Simulation research of the new type actuator based on giant magnetostrictive material
2004, 18(4): 20-23. doi: 10.3969/j.issn.1672-9897.2004.04.005
Abstract(74) PDF(3)
Abstract:
Buffet onset measurement technique for aircraft model in 2.4m wind tunnel
2004, 18(4): 24-27,33. doi: 10.3969/j.issn.1672-9897.2004.04.006
Abstract(110) PDF(7)
Abstract:
Integrative design of supersonic inlet and missile body
2004, 18(4): 28-33. doi: 10.3969/j.issn.1672-9897.2004.04.007
Abstract(174) PDF(2)
Abstract:
Investigation of civil airplane force measurement in low speed wind tunnel
2004, 18(4): 34-37. doi: 10.3969/j.issn.1672-9897.2004.04.008
Abstract(84) PDF(3)
Abstract:
The visualization of vortex field of unsteady motion for 2 - D airfoil--2 pitching motion and heaving/pitching composite motion
2004, 18(4): 38-42,57. doi: 10.3969/j.issn.1672-9897.2004.04.009
Abstract(94) PDF(3)
Abstract:
Research on the tests technology at high angles of attack in 2.4m transonic wind tunnel
2004, 18(4): 43-48. doi: 10.3969/j.issn.1672-9897.2004.04.010
Abstract(122) PDF(3)
Abstract:
Investigation of two special CTS test techniques
2004, 18(4): 49-53. doi: 10.3969/j.issn.1672-9897.2004.04.011
Abstract(80) PDF(2)
Abstract:
Investigation of test method for air pressure height system
2004, 18(4): 54-57. doi: 10.3969/j.issn.1672-9897.2004.04.012
Abstract(1643) PDF(2)
Abstract:
Experimental technique study of supersonic windy fuze dynamotor
2004, 18(4): 58-61. doi: 10.3969/j.issn.1672-9897.2004.04.013
Abstract(101) PDF(2)
Abstract:
Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results
2004, 18(4): 62-66. doi: 10.3969/j.issn.1672-9897.2004.04.014
Abstract(120) PDF(4)
Abstract:
Investigation of dynamic test technology for a model pitching oscillation with large amplitude in high speed wind tunnels
2004, 18(4): 67-71,77. doi: 10.3969/j.issn.1672-9897.2004.04.015
Abstract(92) PDF(4)
Abstract:
The unsteadiness study of nose vortices in the flow over slender body at high angles of attack
2004, 18(4): 72-77. doi: 10.3969/j.issn.1672-9897.2004.04.016
Abstract(84) PDF(3)
Abstract:
Investigation on the low Reynolds number characteristics of the lift and drag of low aspect ratio wings
2004, 18(4): 78-82. doi: 10.3969/j.issn.1672-9897.2004.04.017
Abstract(106) PDF(5)
Abstract:
Dynamic pressure measurements on a delta wing in unsteady free stream
2004, 18(4): 83-87. doi: 10.3969/j.issn.1672-9897.2004.04.018
Abstract(121) PDF(7)
Abstract:
Study on the field of swirler
2004, 18(4): 88-92. doi: 10.3969/j.issn.1672-9897.2004.04.019
Abstract(101) PDF(5)
Abstract:
Investigation on the entropies and chaos characteristics of the instantaneous concentration field
2004, 18(4): 93-98,104. doi: 10.3969/j.issn.1672-9897.2004.04.020
Abstract(115) PDF(3)
Abstract:
Analysis of operative principles of calibration tank in CARIA and acquired methods of objective parameters in TPS calibration
2004, 18(4): 99-104. doi: 10.3969/j.issn.1672-9897.2004.04.021
Abstract(111) PDF(2)
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