Active Control of Disturbances in a Hypersonic Shock Layer
Keyword(s):
The experimental method and devices allowing to realize interference principle of active control of pulsations intensity in a hypersonic shock layer on flat plate in flow of nitrogen at Mach-number M∞ = 21 are described. The results of measurements of disturbances characteristics and results of realization of interference process in the wind tunnel experiment are compared with the data of direct numerical simulation on the basis of full unsteady Navie-Stocks equations.
Keyword(s):
1999 ◽
Vol 40
(6)
◽
pp. 1029-1035
Keyword(s):
2004 ◽
Vol 39
(2)
◽
pp. 181-188
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Keyword(s):
2000 ◽
Vol 412
◽
pp. 259-277
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Keyword(s):
2004 ◽
Vol 332
(11)
◽
pp. 875-880
◽
2000 ◽
pp. 494-500