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Systematic two-dimensional cascade tests. Volume 3: Slotted double circular-arc hydrofoilsPerformance parameters are presented for cascades of slotted double circular-arc hydrofoils tested over a range of systematically introduced variables in a rectilinear cascade tunnel which uses water as the test medium. Cascade configurations included various combinations of an inlet flow angle of 50, 60 and 70 deg; a cascade solidity of 0.75, 1.00 and 1.50; a hydrofoil camber angle of 20, 30, 40 and 45 deg; and angles of incidence between positive and negative stall. The slot was positioned at the 45 percent chord station and the slot exit width was 0.047-in. Tests were also performed with the slot positioned at the 35 percent chord station and with slot widths of 0.63 and 0.094-in. These data were correlated to indicate the effects of slot location and slot width on minimum loss incidence and deviation angles. In addition, a comparison is presented of the performance parameters for cascades of slotted and unslotted hydrofoils.
Document ID
19720016716
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Columbo, R. M.
(United Aircraft Corp. East Hartford, CT, United States)
Murrin, T. A.
(United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
UARL-L930845-81-VOL-3
NASA-CR-72870
Report Number: UARL-L930845-81-VOL-3
Report Number: NASA-CR-72870
Accession Number
72N24366
Funding Number(s)
CONTRACT_GRANT: NAS3-4148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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