2004 No. 2

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Display Method:
Technical ways to solve high speed key aerodynamic problems of large air transporters
2004, 18(2): 1-5. doi: 10.3969/j.issn.1672-9897.2004.02.001
Abstract(94) PDF(2)
Abstract:
A base code for aircraft synthetic design and evaluation
2004, 18(2): 6-10. doi: 10.3969/j.issn.1672-9897.2004.02.002
Abstract(97) PDF(2)
Abstract:
A summary of wind tunnel test techniques for high-altitude long-endurance UAV
2004, 18(2): 11-16. doi: 10.3969/j.issn.1672-9897.2004.02.003
Abstract(80) PDF(7)
Abstract:
Pressure transient analysis and control of water hammer device
2004, 18(2): 17-19,24. doi: 10.3969/j.issn.1672-9897.2004.02.004
Abstract(65) PDF(2)
Abstract:
Test technique of hinge-moment in 8m × 6m wind tunnel
2004, 18(2): 20-24. doi: 10.3969/j.issn.1672-9897.2004.02.005
Abstract(103) PDF(4)
Abstract:
Study on flow characteristics over air refueling tubes
2004, 18(2): 25-27,54. doi: 10.3969/j.issn.1672-9897.2004.02.006
Abstract(92) PDF(2)
Abstract:
The design and calibration of ejected engine simulator
2004, 18(2): 28-31. doi: 10.3969/j.issn.1672-9897.2004.02.007
Abstract(105) PDF(4)
Abstract:
Discussion on the simulation of atmospheric boundary layer with spires and roughness elements in wind tunnels
2004, 18(2): 32-37. doi: 10.3969/j.issn.1672-9897.2004.02.008
Abstract(151) PDF(11)
Abstract:
Correlation investigation of unsteady aerodynamics of dynamic delta wings and pressure distribution
2004, 18(2): 38-42. doi: 10.3969/j.issn.1672-9897.2004.02.009
Abstract(86) PDF(2)
Abstract:
The wind tunnel experiment techniques of backward dispersion of turning shrapnel
2004, 18(2): 43-46. doi: 10.3969/j.issn.1672-9897.2004.02.010
Abstract(104) PDF(4)
Abstract:
The optimization study of optical performance of shear layer in free-vortex ADW
2004, 18(2): 47-49. doi: 10.3969/j.issn.1672-9897.2004.02.011
Abstract(104) PDF(2)
Abstract:
A new approach for experimental model to realize the sinusoidal motions of heaving and pitching in phase
2004, 18(2): 50-54. doi: 10.3969/j.issn.1672-9897.2004.02.012
Abstract(128) PDF(2)
Abstract:
The experiment exploration of catalyst effects on aerodynamic heat in real gas effects
2004, 18(2): 55-58,64. doi: 10.3969/j.issn.1672-9897.2004.02.013
Abstract(135) PDF(3)
Abstract:
An experimental study of turbulent boundary layer over the grooved-surface
2004, 18(2): 59-64. doi: 10.3969/j.issn.1672-9897.2004.02.014
Abstract(83) PDF(3)
Abstract:
The characteristics of nose vortices and Karman vortices in the flow over slender body at high angles of attack
2004, 18(2): 65-70. doi: 10.3969/j.issn.1672-9897.2004.02.015
Abstract(92) PDF(3)
Abstract:
The visualization of vortex field of unsteady motion for 2-D foil--heaving motion
2004, 18(2): 71-76. doi: 10.3969/j.issn.1672-9897.2004.02.016
Abstract(119) PDF(5)
Abstract:
Development on the half model balance in the 2.4 m × 2.4 m transonic wind tunnel
2004, 18(2): 77-81,85. doi: 10.3969/j.issn.1672-9897.2004.02.017
Abstract(112) PDF(7)
Abstract:
Fluid dynamic characteristic measurement of high pressure nozzle used in extinguishing system
2004, 18(2): 82-85. doi: 10.3969/j.issn.1672-9897.2004.02.018
Abstract(89) PDF(2)
Abstract:
Experimental measurements of the turbulence characteristics under sheared air-water interfaces
2004, 18(2): 86-90. doi: 10.3969/j.issn.1672-9897.2004.02.019
Abstract(88) PDF(3)
Abstract:
Section model wind tunnel test for steady aerodynamic force of line-like multi-body system
2004, 18(2): 91-94. doi: 10.3969/j.issn.1672-9897.2004.02.020
Abstract(126) PDF(2)
Abstract:
An algorithm for balance formula
2004, 18(2): 95-97,101. doi: 10.3969/j.issn.1672-9897.2004.02.021
Abstract(81) PDF(2)
Abstract:
The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet
2004, 18(2): 98-101. doi: 10.3969/j.issn.1672-9897.2004.02.022
Abstract(101) PDF(4)
Abstract:

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