Approximate calculation of steady-state shock wave parameters in porous compressible materials

1986 ◽  
Vol 27 (1) ◽  
pp. 107-111 ◽  
Author(s):  
L. G. Gvozdeva ◽  
Yu. M. Faresov
2021 ◽  
Author(s):  
Immanuel Christopher Jebaraj ◽  
Athanasios Kouloumvakos ◽  
Jasmina Magdalenic ◽  
Alexis Rouillard ◽  
Vratislav Krupar ◽  
...  

<p>Eruptive events such as Coronal mass ejections (CMEs) and flares cangenerate shock waves. Tracking shock waves and predicting their arrival at Earth is a subject of numerous space weather studies. Ground-based radio observations allow us to locate shock waves in the low corona while space-based radio observations provide us opportunity to track shock waves in the inner heliosphere. We present a case study of CME/flare event, associated shock wave and its radio signature, i.e. type II radio burst.</p><p>In order to analyze the shock wave parameters, we employed a robust paradigm. We reconstructed the shock wave in 3D using multi-viewpoint observations and modelled the evolution of its parameters using a 3D MHD background coronal model produced by the MAS (Magnetohydrodynamics Around a Sphere).</p><p>To map regions on the shock wave surface, possibly associated with the electron acceleration, we combined 3D shock modelling results with the 3D source positions of the type II burst obtained using the radio triangulation technique. We localize the region of interest on the shock surface and examine the shock wave parameters to understand the relationship between the shock wave and the radio event. We analyzed the evolution of the upstream plasma characteristics and shock wave parameters during the full duration of the type II radio emission. First results indicate that shock wave geometry and its relationship with shock strength play an important role in the acceleration of electrons responsible for the generation of type II radio bursts.</p>


1991 ◽  
pp. 27-32 ◽  
Author(s):  
Emad Fatemi ◽  
Carl L. Gardner ◽  
Joseph W. Jerome ◽  
Stanley Osher ◽  
Donald J. Rose

1998 ◽  
Vol 103 (5) ◽  
pp. 3072-3072 ◽  
Author(s):  
Thomas Dreyer ◽  
Rainer E. Riedlinger ◽  
Eckard Steiger
Keyword(s):  

1966 ◽  
Vol 9 (6) ◽  
pp. 1053 ◽  
Author(s):  
H. L. Frisch
Keyword(s):  

1991 ◽  
Vol 27 (4) ◽  
pp. 438-442 ◽  
Author(s):  
S. P. Medvedev ◽  
A. N. Polenov ◽  
B. E. Gel'fand

1996 ◽  
Vol 118 (2) ◽  
pp. 268-277 ◽  
Author(s):  
A. P. Saxer ◽  
H. M. Felici

A three-dimensional unsteady flow computation has been performed for a transonic first turbine stage under the influence of streaks of hot gas exiting the combustion chamber. Realistic flow conditions are obtained by using an unequal stator-to-rotor pitch, a single-streak/multistator channel configuration, and periodic boundary conditions. The resulting unsteady shock wave system and the hot streak migration as well as the shock wave/streak interaction are presented and discussed. In addition, the time average of the periodic unsteady solution is analyzed and compared with a steady-state computation. The steady-state solution is analyzed and compared with a steady-state computation. The steady-state solution matches the time-averaged one in terms of the pressure field and the maximum stagnation temperature on the rotor blade surface. However, the rotor blade temperature patterns are different with a stronger radial secondary flow present in the time-averaged solution due to the retention of the circumferential streak variations at the stator/rotor interface.


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