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Viscous wing theory development. Volume 2: GRUMWING computer program user's manualThis report is a user's manual which describes the operation of the computer program, GRUMWING. The program computes the viscous transonic flow over three-dimensional wings using a boundary layer type viscid-inviscid interaction approach. The inviscid solution is obtained by an approximate factorization (AFZ)method for the full potential equation. The boundary layer solution is based on integral entrainment methods.
Document ID
19870000611
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chow, R. R. (Grumman Aerospace Corp. Bethpage, NY, United States)
Ogilvie, P. L. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
RE-726-VOL-2
NASA-CR-178157
NAS 1.26:178157
Report Number: RE-726-VOL-2
Report Number: NASA-CR-178157
Report Number: NAS 1.26:178157
Accession Number
87N10044
Funding Number(s)
CONTRACT_GRANT: NAS1-16858
PROJECT: RTOP 505-60-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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