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Calculation of incompressible fluid flow through cambered bladesConformal mapping technique yields linear, approximate solutions for calculating flow of an incompressible fluid through staggered array of cambered blades for the cases of flow with partial cavitation and supercavitation. Lift and drag coefficients, cavitation number, cavity shape, and exit flow conditions can be determined.
Document ID
19700000089
Document Type
Other - NASA Tech Brief
Authors
Hsu, C. C. (HYDRONAUTICS, INC.)
Date Acquired
August 5, 2013
Publication Date
September 1, 1970
Subject Category
MECHANICS
Report/Patent Number
MFS-20503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.