ISBN 9798672401720 is currently unpriced. Please contact us for pricing.
Available options are listed below:
Available options are listed below:
The a(4) Scheme-A High Order Neutrally Stable CESE Solver
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/05/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The CESE development is driven by a belief that a solver should (i) enforce conservation laws in both space and time, and (ii) be built from a nondissipative (i.e., neutrally stable) core scheme so that the numerical dissipation can be controlled effectively. To provide a solid foundation for a systematic CESE development of high order schemes, in this paper we describe a new high order (4-5th order) and neutrally stable CESE solver of a 1D advection equation with a constant advection speed a. The space-time stencil of this two-level explicit scheme is formed by one point at the upper time level and two points at the lower time level. Because it is associated with four independent mesh variables (the numerical analogues of the dependent variable and its first, second, and third-order spatial derivatives) and four equations per mesh point, the new scheme is referred to as the a(4) scheme. As in the case of other similar CESE neutrally stable solvers, the a(4) scheme enforces conservation laws in space-time locally and globally, and it has the basic, forward marching, and backward marching forms. Except for a singular case, these forms are equivalent and satisfy a space-time inversion (STI) invariant property which is shared by the advection equation. Based on the concept of STI invariance, a set of algebraic relations is developed and used to prove the a(4) scheme must be neutrally stable when it is stable. Numerically, it has been established that the scheme is stable if the value of the Courant number is less than 1/3 Chang, Sin-Chung Glenn Research Center NASA/TM-2009-215658, AIAA Paper 2007-5820, E-16100-1 WBS 599489.02.07.03.04.03.01 COMPUTATIONAL GRIDS; SPACE-TIME CE/SE METHOD; INVERSIONS; DEPENDENT VARIABLES; INDEPENDENT VARIABLES; CONSERVATION LAWS; ANALOGS
Show More
Product Format
Product Details
ISBN-13:
9798672401720
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
32
Carton Quantity:
128
Product Dimensions:
8.50 x 0.07 x 11.02 inches
Weight:
0.22 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
The CESE development is driven by a belief that a solver should (i) enforce conservation laws in both space and time, and (ii) be built from a nondissipative (i.e., neutrally stable) core scheme so that the numerical dissipation can be controlled effectively. To provide a solid foundation for a systematic CESE development of high order schemes, in this paper we describe a new high order (4-5th order) and neutrally stable CESE solver of a 1D advection equation with a constant advection speed a. The space-time stencil of this two-level explicit scheme is formed by one point at the upper time level and two points at the lower time level. Because it is associated with four independent mesh variables (the numerical analogues of the dependent variable and its first, second, and third-order spatial derivatives) and four equations per mesh point, the new scheme is referred to as the a(4) scheme. As in the case of other similar CESE neutrally stable solvers, the a(4) scheme enforces conservation laws in space-time locally and globally, and it has the basic, forward marching, and backward marching forms. Except for a singular case, these forms are equivalent and satisfy a space-time inversion (STI) invariant property which is shared by the advection equation. Based on the concept of STI invariance, a set of algebraic relations is developed and used to prove the a(4) scheme must be neutrally stable when it is stable. Numerically, it has been established that the scheme is stable if the value of the Courant number is less than 1/3 Chang, Sin-Chung Glenn Research Center NASA/TM-2009-215658, AIAA Paper 2007-5820, E-16100-1 WBS 599489.02.07.03.04.03.01 COMPUTATIONAL GRIDS; SPACE-TIME CE/SE METHOD; INVERSIONS; DEPENDENT VARIABLES; INDEPENDENT VARIABLES; CONSERVATION LAWS; ANALOGS
Show More
