Intersections of Hugoniot curves with the sonic surface in the wave manifold

2013 ◽  
Vol 44 (2) ◽  
pp. 255-272
Author(s):  
Cesar S. Eschenazi ◽  
Carlos Frederico B. Palmeira
2020 ◽  
Vol 128 (23) ◽  
pp. 235901
Author(s):  
Tie Wei ◽  
Seokbin Lim ◽  
Yanxing Wang
Keyword(s):  

Author(s):  
Christopher R. Johnson ◽  
John P. Borg

Abstract A series of dynamic compaction studies were performed on yttria-stabilized zirconia (YSZ) and graphene composites using uniaxial flyer plate impact experiments. Studies aimed to characterize variation in dynamic behavior with respect to morphological differences for eight powdered YSZ and graphene compositions. Parameters of interest included YSZ particle size (nanometer or micrometer) and added graphene content (graphene weight percentage: 0%, 1%, 3%, 5%). Experiments were performed over impact velocities ranging between 315 and 586 m/s, resulting in pressures between 0.8 and 2.8 GPa. Hugoniot states measured appear to exhibit dependence on particle size and graphene content. Shock velocities tended to increase with graphene content and were generally larger in magnitude for the micrometer particle size YSZ. Compacted densities tended to increase as graphene content was increased and were generally larger in magnitude for the micrometer particle size YSZ samples. Resulting Hugoniot curves are compared and summarized to convey the dynamic behavior of the specimens.


1969 ◽  
Vol 40 (9) ◽  
pp. 3786-3795 ◽  
Author(s):  
P. C. Lysne ◽  
R. R. Boade ◽  
C. M. Percival ◽  
O. E. Jones
Keyword(s):  

2007 ◽  
Vol 19 (47) ◽  
pp. 476218 ◽  
Author(s):  
Aïmen E Gheribi ◽  
Jean-Marc Roussel ◽  
Jacques Rogez

2014 ◽  
Vol 12 (1) ◽  
pp. 5-14
Author(s):  
Jane Grant ◽  
John Matthias ◽  
Simon Honywill
Keyword(s):  

2011 ◽  
Vol 115 (39) ◽  
pp. 10729-10737 ◽  
Author(s):  
Emeric Bourasseau ◽  
Jean-Bernard Maillet ◽  
Nicolas Desbiens ◽  
Gabriel Stoltz

2015 ◽  
Vol 07 (02) ◽  
pp. 1550019 ◽  
Author(s):  
A. Kuzmin

2D and 3D transonic flows in a channel of variable cross-section are studied numerically using a solver based on the Reynolds-averaged Navier–Stokes equations. The flow velocity is supersonic at the inlet and outlet of the channel. Between the supersonic regions, there is a local subsonic region whose upstream boundary is a shock wave, whereas the downstream boundary is a sonic surface. The sonic surface gives rise to an instability of the shock wave position in the channel. Computations reveal a hysteresis in the shock position versus the inflow Mach number. A dependence of the hysteresis on the velocity profile given at the inlet is examined.


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