DocumentCode :
358008
Title :
Unsteadiness of the flow rate of the gas passing through gas-dynamic tracts with contour discontinuities
Author :
Kuraev, A.A. ; Petrov, A.P.
Author_Institution :
Inst. of Theor. & Appl. Mech., Novosibirsk State Tech. Univ., Russia
Volume :
1
fYear :
1999
fDate :
1999
Firstpage :
44
Abstract :
Apart from usual noise caused by a free air stream, the operation of wind tunnels with an open test section is accompanied by the excitation of periodic fluctuations of pressure and flow rate, which increase with the flow velocity. To verify the fact that the vortices pass through the throat, Schlieren pictures of the flow in a plane model were taken. The vortices generated in the subsonic section of the channel come into the throat. For a symmetric inflow, the vortices pass from below and from above with an equal probability. Judging by the behavior of the characteristics passing from the channel generatrices, the velocity of vortices coincides with the flow velocity
Keywords :
channel flow; schlieren systems; vortices; wind tunnels; Schlieren pictures; channel generatrices; contour discontinuities; flow rate unsteadiness; flow velocity; free air stream; gas-dynamic tracts; open test section; periodic fluctuations; plane model; subsonic section; symmetric inflow; vortices; wind tunnels; Amplitude estimation; Character generation; Damping; Fluctuations; Fluid dynamics; Frequency; Jacobian matrices; Large-scale systems; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Science and Technology, 1999. KORUS '99. Proceedings. The Third Russian-Korean International Symposium on
Conference_Location :
Novosibirsk
Print_ISBN :
0-7803-5729-9
Type :
conf
DOI :
10.1109/KORUS.1999.875863
Filename :
875863
Link To Document :
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