2003 No. 4

Display Method:
Investigation of the direction control for the tailless aircraft configuration
2003, 17(4): 1-9. doi: 10.3969/j.issn.1672-9897.2003.04.001
Abstract(93) PDF(3)
Abstract:
Experimental study of Reynolds numbers effect on asymmetric vortices and their aerodynamic characteristics over a slender body
2003, 17(4): 10-16. doi: 10.3969/j.issn.1672-9897.2003.04.002
Abstract(126) PDF(4)
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Numerical simulation of supersonic jets of asymmetric nozzles
2003, 17(4): 17-21. doi: 10.3969/j.issn.1672-9897.2003.04.003
Abstract(96) PDF(4)
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Experimental study on the passive scalar diffusion in shearless turbulent mixing layer
2003, 17(4): 22-27. doi: 10.3969/j.issn.1672-9897.2003.04.004
Abstract(120) PDF(5)
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Influence of wind direction on pressure distributions of adjacent buildings
2003, 17(4): 28-33. doi: 10.3969/j.issn.1672-9897.2003.04.005
Abstract(69) PDF(3)
Abstract:
Wind tunnel experiments were carried out to investigate the influence of wind direction on the wind pressure of proximite buildings.Mean and fluctuating pressure coefficients on a high building,at sixteen different wind incidences and with one and two interfering buildings,were measured in the tests.This paper presents the characteristics of wind pressure on the building,which varies with the incident wind angle and with the numbers of adjacent buildins.Due to the variation of wind angle and the interference effects,the complex feature of pressure distributions can be found on the downstream building surfaces for building group arrangement at certain angle of wind attack.Some area of the interfered building for such configuration,in comparison with one single building's,may undergo very strong positive or negative pressures.
Experimental research of secondary injection based on thrust vector control
2003, 17(4): 34-37. doi: 10.3969/j.issn.1672-9897.2003.04.006
Abstract(87) PDF(4)
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Research of asymmetric vortex characteristic about forebody of slender wing and body
2003, 17(4): 38-42. doi: 10.3969/j.issn.1672-9897.2003.04.007
Abstract(122) PDF(2)
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The series investigations on an aircraft in 4m×3m wind-tunnel
2003, 17(4): 43-47. doi: 10.3969/j.issn.1672-9897.2003.04.008
Abstract(131) PDF(3)
Abstract:
Investigation on dynamic force tests for the stabilizing parachute of the ejection seat in high speed wind tunnel
2003, 17(4): 48-50,55. doi: 10.3969/j.issn.1672-9897.2003.04.009
Abstract(103) PDF(2)
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Preliminary research of infrared thermographic technique in hypersonic low density wind tunnel
2003, 17(4): 51-55. doi: 10.3969/j.issn.1672-9897.2003.04.010
Abstract(133) PDF(7)
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Experimental research of the flow field through porous windbreaks with particle image velocimetry(PIV)
2003, 17(4): 56-61. doi: 10.3969/j.issn.1672-9897.2003.04.011
Abstract(84) PDF(4)
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Ice slurry storage testing technology and its evaluation
2003, 17(4): 62-67. doi: 10.3969/j.issn.1672-9897.2003.04.012
Abstract(136) PDF(2)
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The application of particle image velocimetry to fluid experimentation in a turbine cascade
2003, 17(4): 68-70,83. doi: 10.3969/j.issn.1672-9897.2003.04.013
Abstract(110) PDF(14)
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Visualizations of horseshoe vortex structure
2003, 17(4): 71-78. doi: 10.3969/j.issn.1672-9897.2003.04.014
Abstract(141) PDF(7)
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A visualization study of the instantaneous flow patterns in a laminar junction flow is presented in the paper. The pulsed hydrogen bubble technique and video recording system allows the recording of instantaneous flow field in the present study. The arrangement of the hydrogen bubble wire was proven to be critical for revealing the fine structure of the junction flow. The junction flows produced by a rectangular block extending from the surface were tested with Reynolds number ranging from Reδ* = 2.74 × 102 to 3.19 × 102. The results illustrate the existence of primary horseshoe vortices and counter-rotating secondary vortices. Some new features, such as the behavior of the head portion of a primary HV in the formation region and its shoulders upstream of the block, were found in the visualization study.
Dispenser radar cross section computation and measurement
2003, 17(4): 79-83. doi: 10.3969/j.issn.1672-9897.2003.04.015
Abstract(91) PDF(2)
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Micro-PIV system and its realization
2003, 17(4): 84-88. doi: 10.3969/j.issn.1672-9897.2003.04.016
Abstract(104) PDF(6)
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The development of test management software based on centralized distributed measurement and control LAN
2003, 17(4): 89-91,95. doi: 10.3969/j.issn.1672-9897.2003.04.017
Abstract(110) PDF(3)
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A database management system for low speed wind tunnels
2003, 17(4): 92-95. doi: 10.3969/j.issn.1672-9897.2003.04.018
Abstract(122) PDF(6)
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Method study on wing-body interference coefficient for missiles with arbitrary shape cross section
2003, 17(4): 96-98. doi: 10.3969/j.issn.1672-9897.2003.04.019
Abstract(102) PDF(2)
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