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