NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
2nd-Order CESE Results For C1.1: Transonic Ringleb FlowThe Conservation Element and Solution Element (CESE) method was used as implemented in the NASA research code ez4d (an unstructured Navier-Stokes solver coded in C++ with serial and parallel versions available.) The CESE method is a time-accurate formulation with flux-conservation in both space and time. The method treats the discretized derivatives of space and time identically and while the 2nd-order accurate version was used, high-order versions exist.
Document ID
20150002104
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Friedlander, David J. (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 25, 2015
Publication Date
January 3, 2015
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Computer Programming And Software
Report/Patent Number
GRC-E-DAA-TN19519
Report Number: GRC-E-DAA-TN19519
Meeting Information
Meeting: International Workshop on High-Order CFD Methods
Location: Kissimmee, FL
Country: United States
Start Date: January 3, 2015
End Date: January 4, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, NASA Headquarters, Deutsches Zentrum fuer Luft- und Raumfahrt e.V., Army Research Office
Funding Number(s)
WBS: WBS 794072.02.03.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Numerical Analysis
Space-Time CE/SE Method
Computational Fluid Dynamics

Related Records

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