NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of the cross flow in a radial inflow turbine scrollEquations of motion were derived, and a computational procedure is presented, for determining the nonviscous flow characteristics in the cross-sectional planes of a curved channel due to continuous mass discharge or mass addition. An analysis was applied to the radial inflow turbine scroll to study the effects of scroll geometry and the through flow velocity profile on the flow behavior. The computed flow velocity component in the scroll cross-sectional plane, together with the through flow velocity profile which can be determined in a separate analysis, provide a complete description of the three dimensional flow in the scroll.
Document ID
19780011210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hamed, A.
(Cincinnati Univ. OH, United States)
Abdallah, S.
(Cincinnati Univ. OH, United States)
Tabakoff, W.
(Cincinnati Univ. OH, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135320
Report Number: NASA-CR-135320
Accession Number
78N19153
Funding Number(s)
CONTRACT_GRANT: NSG-3066
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available