NASA NTRS · 19870000611
Viscous wing theory development. Volume 2: GRUMWING computer program user's manual
Abstract
This 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.
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Chow, R. R., Ogilvie, P. L.. 1986-10-01. Viscous wing theory development. Volume 2: GRUMWING computer program user's manual. https://ntrs.nasa.gov/citations/19870000611
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