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A Brief Note on the Interaction of an Actuator Cascade with a Singularity

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Title A Brief Note on the Interaction of an Actuator Cascade with a Singularity
 
Creator Chamieh, D.
Acosta, A. J.
Brennen, C. E.
Caughey, T. K.
 
Subject Caltech Library Services
 
Description We have recently become concerned with making estimates of steady forces that may be exerted between moving blade rows and stationary blade rows or volutes. Our present interest is with time averaged forces for estimation of shaft loads and flow asymmetry forces rather than with transient processes. For this purpose we have adopted the well-known "actuator" model for the blade row in which the flow leaving the row or cascade is assumed to have a constant leaving angle. The disturbances external to this row such as a volute may be represented by distributions of vortex elements as was done for example by Domm and Hergt [1].
 
Publisher National Aeronautics and Space Administration
 
Contributor Childs, Dara W.
Hendricks, Robert C.
Vance, John M.
 
Date 1980
 
Type Book Section
PeerReviewed
 
Format application/pdf
 
Identifier http://authors.library.caltech.edu/203/1/CHA044.pdf
Chamieh, D. and Acosta, A. J. and Brennen, C. E. and Caughey, T. K. (1980) A Brief Note on the Interaction of an Actuator Cascade with a Singularity. In: Rotordynamic Instability Problems in High-Performance Turbomachinery. NASA Conference Publication. No.CP-2133. National Aeronautics and Space Administration , Washington, DC, USA, pp. 237-248. http://resolver.caltech.edu/CaltechAUTHORS:CHAriphpt80 <http://resolver.caltech.edu/CaltechAUTHORS:CHAriphpt80>
 
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http://authors.library.caltech.edu/203/