- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- The numerical scheme presented belongs to a family of codes known as UNCLE (UNsteady Computation of fieLd Equations) as reported by Whitfield (1995), that is being used to solve problems in a variety of areas including compressible and incompressible flows. This derivation is specifically developed for general unsteady multi-blade-row turbomachinery problems. The scheme solves the Reynolds-averaged N-S equations with the Baldwin-Lomax turbulence model.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19960008849.
Accession ID: 96N16015.
- No Copyright.
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