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Shock formation in a poloidally rotating tokamak plasma

Technical Report ·
OSTI ID:5372476
 [1];  [2];  [3]
  1. Oak Ridge National Lab., TN (United States)
  2. Texas Univ., Austin, TX (United States). Inst. for Fusion Studies
  3. National Inst. for Fusion Science, Nagoya (Japan)
When the Mach number M{sub p} of the poloidal rotation in a tokamak approaches unity, the poloidal variations of plasma density and potential appear to have the characteristics of a shock whose front lies on a plane (ribbon) of a fixed poloidal angle {eta}{sub 0}. The shock first appears, when 1 {minus} Mp {approx lt} {radical}{bar {epsilon}} ({epsilon} is the inverse aspect ratio), on the inside of the torus at a shock angle {eta}{sub 0} {ge} {pi} if the plasma rotates counterclockwise poloidally. As M{sub p} increases, {eta}{sub 0} moves in the direction of the poloidal rotation. At M{sub p} = 1, {eta}{sub 0} = 2{pi}. When M{sub p} {minus} {approx lt} {radical}{bar {epsilon}}, the shock angle is at {eta}{sub 0} {approx lt} {pi}. The parallel viscosity associated with the shock is collisionality independent, in contrast to the conventional neoclassical viscosity. The viscosity reaches its maximum at M{sub p} = 1, which is the barrier that must be overcome to have a poloidal supersonic flow. Strong up-down asymmetric components of poloidal variations of plasma density and potential develop at M{sub p} {approx equal} 1. In the edge region, the convective poloidal momentum transport weakens the parallel viscosity and facilitates the transition from L-mode to H-mode. 24 refs., 2 figs.
Research Organization:
Texas Univ., Austin, TX (United States). Inst. for Fusion Studies; Oak Ridge National Lab., TN (United States)
Sponsoring Organization:
DOE; USDOE, Washington, DC (United States)
DOE Contract Number:
FG05-80ET53088; AC05-84OR21400
OSTI ID:
5372476
Report Number(s):
DOE/ET/53088-505; IFSR--505; ON: DE91018417
Country of Publication:
United States
Language:
English