Publication Date:
2019-07-12
Description:
The 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.
Keywords:
Numerical Analysis; Astronautics (General)
Type:
NASA/TM-2015-218743
,
E-19071
,
GRC-E-DAA-TN21438
Format:
application/pdf
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