2003 No. 2

Display Method:
Unsteady aerodynamics in fatal accidents
2003, 17(2): 1-9. doi: 10.3969/j.issn.1672-9897.2003.02.001
Abstract(90) PDF(2)
Abstract:
Cold flow experimental study of plug nozzle
2003, 17(2): 10-14. doi: 10.3969/j.issn.1672-9897.2003.02.002
Abstract(127) PDF(3)
Abstract:
Application of PIV technique in unsteady characteristics research of streak wing leading vortex
2003, 17(2): 15-18. doi: 10.3969/j.issn.1672-9897.2003.02.003
Abstract(64) PDF(6)
Abstract:
Zonal study of flow patterns around an ogive-cylinder at subcritical Reynolds nmnbers
2003, 17(2): 19-25,36. doi: 10.3969/j.issn.1672-9897.2003.02.004
Abstract(112) PDF(3)
Abstract:
Investigation of the arrow wing aerodynamic performance
2003, 17(2): 26-31. doi: 10.3969/j.issn.1672-9897.2003.02.005
Abstract(88) PDF(4)
Abstract:
The experimental investigation of effects of entry forms on inlet properties at low speed
2003, 17(2): 32-36. doi: 10.3969/j.issn.1672-9897.2003.02.006
Abstract(75) PDF(2)
Abstract:
Investigation of support interference in low speed wind tunnel oscillation tests
2003, 17(2): 37-40. doi: 10.3969/j.issn.1672-9897.2003.02.007
Abstract(79) PDF(2)
Abstract:
Experimental investigation of the vortex characteristic over 75°/45° double delta wing
2003, 17(2): 41-44. doi: 10.3969/j.issn.1672-9897.2003.02.008
Abstract(118) PDF(2)
Abstract:
The research of civil aircraft afterbody test technique
2003, 17(2): 45-48. doi: 10.3969/j.issn.1672-9897.2003.02.009
Abstract(127) PDF(2)
Abstract:
Wind tunnel research on statics thrust characteristics of vectoring nozzle
2003, 17(2): 49-53. doi: 10.3969/j.issn.1672-9897.2003.02.010
Abstract(93) PDF(3)
Abstract:
Research of the vortex-shedding frequency characteristics in the annular cascade
2003, 17(2): 54-58. doi: 10.3969/j.issn.1672-9897.2003.02.011
Abstract(106) PDF(2)
Abstract:
The design and experimental investigations of supersonic free-vortex ADW
2003, 17(2): 59-62,69. doi: 10.3969/j.issn.1672-9897.2003.02.012
Abstract(120) PDF(2)
Abstract:
Aerodynamic experimental investigation in blade erosion of gas-solid two-phase turbine
2003, 17(2): 63-69. doi: 10.3969/j.issn.1672-9897.2003.02.013
Abstract(101) PDF(3)
Abstract:
The comparison between two deploying methods and results of folding wings for some tactical missiles
2003, 17(2): 70-73. doi: 10.3969/j.issn.1672-9897.2003.02.014
Abstract(95) PDF(4)
Abstract:
Flow visualization about a compressible shear flow
2003, 17(2): 74-77,83. doi: 10.3969/j.issn.1672-9897.2003.02.015
Abstract(87) PDF(2)
Abstract:
A new transportation method for heavy oil by steam injector
2003, 17(2): 78-83. doi: 10.3969/j.issn.1672-9897.2003.02.016
Abstract(96) PDF(3)
Abstract:
Study on flow characteristics and noise mechanics of impinging jet with high speed
2003, 17(2): 84-87. doi: 10.3969/j.issn.1672-9897.2003.02.017
Abstract(134) PDF(5)
Abstract:
The research of DPIV system and its application
2003, 17(2): 88-92. doi: 10.3969/j.issn.1672-9897.2003.02.018
Abstract(94) PDF(2)
Abstract:
Towing PIV technique and its application in a tank
2003, 17(2): 93-97. doi: 10.3969/j.issn.1672-9897.2003.02.019
Abstract(111) PDF(5)
Abstract:
The influences of time lag dynamic derivatives on the evaluation of the spin time history of a modified airplane
2003, 17(2): 98-102. doi: 10.3969/j.issn.1672-9897.2003.02.020
Abstract(94) PDF(2)
Abstract: