shock impingement
Recently Published Documents


TOTAL DOCUMENTS

53
(FIVE YEARS 15)

H-INDEX

9
(FIVE YEARS 2)

2022 ◽  
Author(s):  
Patrick Cragg ◽  
Friedolin T. Strauss ◽  
Stephan General ◽  
Stefan Schlechtriem

2021 ◽  
Vol 33 (10) ◽  
pp. 105104
Author(s):  
Zhigang Zhang ◽  
Fulin Tong ◽  
Junyi Duan ◽  
Xinliang Li

2021 ◽  
Author(s):  
Jianjun Liu

<p>Interplanetary (IP) shock driven sudden compression produces disturbances in the polar ionosphere. Various studies have investigated the effects of IP shock using imagers and radars. However, very few studies have reported the plasma flow reversal and a sudden vertical plasma drift motion following a CME driven IP shock. We report on the cusp ionospheric features following an IP shock impingement on 16 June 2012, using SuperDARN radar and digisonde from the Antarctic Zhongshan Station (ZHO). SuperDARN ZHO radar observed instant strong plasma flow reversal during the IP shock driven sudden impulse (SI) with a suppression in the number of backscatter echoes. Besides, we also report on a “Doppler Impulse” phenomenon, an instant and brief downward plasma motion, were observed by the digisonde in response to the SI and discuss the possible physical causes. Geomagnetic disturbance and convection patterns indicate the flow reversal was generated by the downward field-aligned current (FAC). We speculate that sudden enhancement in ionization associated with SI is responsible for generating the Doppler Impulse phenomenon.</p>


2021 ◽  
Author(s):  
Kirk R. Brouwer ◽  
Ricardo Perez ◽  
Timothy J. Beberniss ◽  
Stephen M. Spottswood ◽  
David A. Ehrhardt

2020 ◽  
Vol 908 ◽  
Author(s):  
Eric Won Keun Chang ◽  
Wilson Y. K. Chan ◽  
Timothy J. McIntyre ◽  
Ananthanarayanan Veeraragavan

Abstract


2020 ◽  
pp. 2150059
Author(s):  
Junhong Feng ◽  
Junyong Lu ◽  
Chibing Shen

Vorticity variation in a supersonic planar mixing layer interacting with an oblique shock wave is investigated analytically and numerically. A model that simplifies the mixing layer to a discontinuous flow is established to solve the post-shock flow parameters, and it is validated through qualitative and quantitative comparisons with the Buttsworth’s model and numerical results. A model to estimate the shock-induced Maximum Vorticity Amplification (MVA) is obtained, which agrees well with the numerical results. The model could estimate the growth rate and maximum vorticity of the shocked mixing layer. The vorticity of the mixing layer is amplified by the shock impingement, even though the vorticity thickness decreases, which can improve the mixing performance for different practical applications.


Sign in / Sign up

Export Citation Format

Share Document