scholarly journals Direct Numerical Simulation of Acoustic Noise Generation from the Nozzle Wall of a Hypersonic Wind Tunnel

Author(s):  
Junji Huang ◽  
Lian Duan
1994 ◽  
Vol 60 (580) ◽  
pp. 4082-4088
Author(s):  
Takashi Kawashima ◽  
Hidenori Yoshida ◽  
Hiromitsu Kiyose ◽  
Hideki Kawamoto

2008 ◽  
Vol 3 (2) ◽  
pp. 15-20
Author(s):  
Sergey G. Mironov ◽  
Anatoliy Maslov ◽  
Alexey N. Kudryavtsev ◽  
Tatyana V. Poplavskaya ◽  
Ivan S. Tsyryulnikov

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.


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