The influence of tip clearance on stall limits of a rectilinear cascade of compressor blades

August 1959

Bibliographic Details
Main Author:	Khabbaz, Ghassan R. (Ghassan Raji)
Other Authors:	Massachusetts Institute of Technology. Gas Turbine Laboratory
Format:	Technical Report
Published:	Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959] 2016
Subjects:	TJ267.A1 M37 no.54 Cascades (Fluid dynamics) Compressors > Blades Aerodynamic load
Online Access:	http://hdl.handle.net/1721.1/104673

Internet

http://hdl.handle.net/1721.1/104673