Computer code written to analyze flows on blade-to-blade surfaces of turbomachinery. Analyzes rows containing blades of several different shapes and/or spacings. Capability makes code useful for calculating flows in centrifugal machinery with splitter blades or in mistuned blade rows, where blade spacing varies. Written primarily in FORTRAN IV.
Calculating Flows In Multiple-Blade-Element Cascades
NASA Tech Briefs ; 12 , 1
1988-01-01
Sonstige
Keine Angabe
Englisch
FLUID DYNAMICS - Unsteady Swirling Flows in Annular Cascades, Part 2: Aerodynamic Blade Response
Online Contents | 2000
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