Published January 1989 | Version v1
Journal article

Rippled shock front solutions for testing hydrodynamic stability simulations

Creators

  • 1. Lawrence Livermore National Laboratory, Livermore, California 94550

Description

The response of a shock front to arbitrary small perturbations can be calculated analytically. Such rippled shock front solutions are useful for determining the accuracy of hydrodynamic simulation codes such as LASNEX [Comments Plasma Phys. Controlled Fusion 2, 51 (1977)], which are used to compute perturbation growth in inertial fusion targets. The LASNEX fractional errors are of order κ2L2, where κ is the transverse wavenumber of the perturbation, and L is the largest zone dimension. Numerical errors are about 25% for a calculation using 26 zones per transverse wavelength

Additional details

Publishing Information

Journal Title
Physics of Fluids B
Journal Volume
1
Journal Issue
1
Series
Phys. Fluids B.
Journal Page Range
134-141
CODEN
PFBPE

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
20039056
Subject category
S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
Resource subtype / Literary indicator
Numerical Data
Descriptors DEI
ANALYTICAL SOLUTION; DISPERSION RELATIONS; DISTURBANCES; ERRORS; HYDRODYNAMICS; INERTIAL CONFINEMENT; INSTABILITY GROWTH RATES; NUMERICAL DATA; PLASMA; SHOCK WAVES; SIMULATION
Descriptors DEC
CONFINEMENT; DATA; FLUID MECHANICS; INFORMATION; MECHANICS; PLASMA CONFINEMENT