Study of secondary-flow patterns in an annular cascade of turbine nozzle blades with vortex design / Harold E. Rohlik, Hubert W. Allen, and Howard Z. Herzig.

In order to increase understanding of the origin of losses in a turbine, the secondary-flow components in the boundary layers and the blade wakes of an annular cascade of turbine nozzle blades (vortex design) were investigated. A detailed study was made of the total-pressure contours and, particular...

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Main Author: Rohlik, Harold E.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Allen, Hubert W., Herzig, Howard Z.
Other title:Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1953.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2909.
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Call Number: Y 3.N 21/5:6/2909
Y 3.N 21/5:6/2909 Available Place a Hold