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GRUMFOIL: A computer code for the viscous transonic flow over airfoilsA user's manual which describes the operation of the computer program, GRUMFOIL is presented. The program computes the viscous transonic flow over two dimensional airfoils using a boundary layer type viscid-inviscid interaction approach. The inviscid solution is obtained by a multigrid method for the full potential equation. The boundary layer solution is based on integral entrainment methods.
Document ID
19860002735
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mead, H. R.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Melnik, R. E.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3806
RE-681
NAS 1.26:3806
Accession Number
86N12202
Funding Number(s)
CONTRACT_GRANT: NAS1-12426
PROJECT: RTOP 505-31-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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