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Boundary layer transition detection on blade surface in low soeed turbine cascade wind tunnel
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2003, 17(1): 1-5. DOI: 10.3969/j.issn.1672-9897.2003.01.001
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The balance test in shock tunnel for the war-head with ablation nose
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2003, 17(1): 6-8,14. DOI: 10.3969/j.issn.1672-9897.2003.01.002
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Impulse calculation of no- restriction touch blasting with geometry analysis
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2003, 17(1): 9-14. DOI: 10.3969/j.issn.1672-9897.2003.01.003
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The research and application of phase change thermography technique
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2003, 17(1): 15-17,23. DOI: 10.3969/j.issn.1672-9897.2003.01.004
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Research on the effects of unsteady excitation on enhancing performance of annular cascade
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2003, 17(1): 18-23. DOI: 10.3969/j.issn.1672-9897.2003.01.005
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The realization of CTS test with control law
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2003, 17(1): 24-27. DOI: 10.3969/j.issn.1672-9897.2003.01.006
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A study on the optimization for the protective atmosphere of pins in hydrodynamic measurements
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2003, 17(1): 28-31. DOI: 10.3969/j.issn.1672-9897.2003.01.007
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A new control system of CTS device and its application in 1.2m high speed wind tunnel
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2003, 17(1): 32-35. DOI: 10.3969/j.issn.1672-9897.2003.01.008
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Investigation of the method for gain M ≥ 1 uniform transonic flow field at a special wind tunnel condition
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2003, 17(1): 36-38. DOI: 10.3969/j.issn.1672-9897.2003.01.009
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Experimental investigation on aircraft component and external-stores force-measurement in high speed wind tunnel
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2003, 17(1): 39-42,50. DOI: 10.3969/j.issn.1672-9897.2003.01.010
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VISAR used in exposive reaction zone measuement
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2003, 17(1): 43-45. DOI: 10.3969/j.issn.1672-9897.2003.01.011
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Investigation of real train test into the pressure distribution on external surface of the electric passenger train of scattered power at a speed of 200km/h
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2003, 17(1): 46-50. DOI: 10.3969/j.issn.1672-9897.2003.01.012
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The counter design and flow analysis of axial-symmetric length-shorted nozzle
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2003, 17(1): 51-54. DOI: 10.3969/j.issn.1672-9897.2003.01.013
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The experimental study for wake characteristic of the refueling airplane model
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2003, 17(1): 55-58. DOI: 10.3969/j.issn.1672-9897.2003.01.014
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Visualization experiments of flow field in stratified atmospheres over complex terrain
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2003, 17(1): 59-63. DOI: 10.3969/j.issn.1672-9897.2003.01.015
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Pressure measurement inside and outside the vessel during venting explosions
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2003, 17(1): 64-67. DOI: 10.3969/j.issn.1672-9897.2003.01.016
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The exploration of a new kind of free-released balance in impulsive wind tunnels
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2003, 17(1): 68-72. DOI: 10.3969/j.issn.1672-9897.2003.01.017
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Measure of flux for base bleed wind tunnel experiment
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2003, 17(1): 73-75. DOI: 10.3969/j.issn.1672-9897.2003.01.018
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The investigation of pipe flow condition requirments for gas flow rate measurement
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2003, 17(1): 76-79. DOI: 10.3969/j.issn.1672-9897.2003.01.019
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Digitalization and analysis of hydrogen-bubble visualized flow structures
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2003, 17(1): 80-83. DOI: 10.3969/j.issn.1672-9897.2003.01.020
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The study for the wake model of wind turbine and the wake effects on the performance of wind turbine
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2003, 17(1): 84-87. DOI: 10.3969/j.issn.1672-9897.2003.01.021
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The study of one-dimensional flow analysis model of the combustor in supersonic combustion experiments
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2003, 17(1): 88-92. DOI: 10.3969/j.issn.1672-9897.2003.01.022
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