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A gridless Euler/Navier-Stokes solution algorithm for complex-aircraft applicationsThe development of a gridless computational fluid dynamics (CFD) method for the solution of the two- and three-dimensional Euler and Navier-Stokes equations is described. The method uses only clouds of points and does not require that the points be connected to form a grid as is necessary in conventional CFD algorithms. The gridless CFD approach appears to resolve the inefficiencies encountered with structured or unstructured grid methods, and consequently offers great potential for accurately and efficiently solving viscous flows about complex aircraft configurations. The method is described in detail and calculations are presented for standard Euler and Navier-Stokes cases to assess the accuracy and efficiency of the capability.
Document ID
19930010784
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Batina, John T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-107727
NAS 1.15:107727
Report Number: NASA-TM-107727
Report Number: NAS 1.15:107727
Meeting Information
Meeting: AIAA 31st Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Accession Number
93N19973
Funding Number(s)
PROJECT: RTOP 505-63-50-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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