Simulations of a Normal Shock Train in a Constant Area Duct Using Wall-Modeled LES

Author(s):  
Zachary P. Vane ◽  
Sanjiva K. Lele
AIAA Journal ◽  
2014 ◽  
Vol 52 (3) ◽  
pp. 539-558 ◽  
Author(s):  
Brandon Morgan ◽  
Karthik Duraisamy ◽  
Sanjiva K. Lele

2018 ◽  
Vol 180 ◽  
pp. 02063
Author(s):  
Atsushi Matsuyama ◽  
Shinichiro Nakao ◽  
Daisuke Ono ◽  
Yoshiaki Miyazato ◽  
Masashi Kashitani

The rainbow schlieren deflectometry is effective in studying quantitatively the density fields in shock-containing free jets at high precision and high spatial resolution. However, there has been no practical application of rainbow schlieren deflectometry for shock trains in a confined duct. Therefore, in the present study, the rainbow schlieren deflectometry is applied to the flow field including a shock train in a constant-area duct where just upstream of the shock train the freestream Mach number is 1.34, the unit Reynolds number is 5.39 × 107 m-1, and the boundary layer displacement thickness is 0.149 mm. As a result, a two- dimensional density field of the shock train is for the first time quantitatively displayed and the fine structure of the shock train is illustrated as a color gradation representation.


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