NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A Summary of the Space-Time Conservation Element and Solution Element (CESE) MethodThe space-time Conservation Element and Solution Element (CESE) method for solving conservation laws is examined for its development motivation and design requirements. The characteristics of the resulting scheme are discussed. The discretization of the Euler equations is presented to show readers how to construct a scheme based on the CESE method. The differences and similarities between the CESE method and other traditional methods are discussed. The strengths and weaknesses of the method are also addressed.
Document ID
20160001345
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Wang, Xiao-Yen J. (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 2, 2016
Publication Date
June 1, 2015
Subject Category
Numerical Analysis
Astronautics (General)
Report/Patent Number
GRC-E-DAA-TN21438
E-19071
NASA/TM-2015-218743
Report Number: GRC-E-DAA-TN21438
Report Number: E-19071
Report Number: NASA/TM-2015-218743
Funding Number(s)
WBS: WBS 109492.02.03.01.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Fluid Dynamics
Aerodynamics
Numerical Methods

Related Records

There are no records associated with this record.
No Preview Available