Blade row interference in axial turbomachinery stages - hardcover - VKI LS 1998-02

Blade row interference in axial turbomachinery stages
February 9-12, 1998; C.H. Sieverding & H.P. Hodson

Table of contents

• HODSON, H.P. - Whittle Laboratory, University of Cambridge, United Kingdom
  Blade row interactions in low pressure turbines
• DAWES, W.N. - Cambridge University, Engineering Dept., United Kingdom
  Simulation of unsteady blade row interaction with CFD: applications
  Simulation of unsteady blade row interaction with CFD: background
• LESCHZINER, M.A. - Univ. of Manchester, Institute of Science and Technology, United Kingdom
  Turbulence modelling for physically complex flows pertinent to turbomachine aerodynamics
• SIEVERDING, C.H.; DENOS, R.; ARTS, T.; BROUKCKAERT, J.-F.; PANIAGUA, G. - von Karman Institute, Belgium
  Experimental investigation of the unsteady rotor aerodynamics and heat transfer of a transonic turbine stage
• MICHELASSI, V. & MARTELLI, F. - University of Florence, Italy
  Numerical simulation of unsteady stator-rotor interaction in Brite-turbine stage
• WISLER, C. & SHIN, H-W. - GE Aircraft Engines, Cincinnati, USA
  Blade row interaction and unsteady effects in axial-flow compressors and fans
• WISLER, C. - GE Aircraft Engines, Cincinnati, USA
  The technical and economic relevance of understanding blade row interaction effects in turbomachinery
• SHARMA, O.¹ & TAN, C.S.² - ¹Pratt & Whitney, Esat Hartford, USA & ²Gas Turbine Laboratory, MIT, United Kingdom
  Impact of unsteadiness induced by adjacent airfoils rows on the performance, structural integrity and stalling characteristics of axial flow compressors
• SHARMA, O.P. & STETSON, G.M. - Pratt & Whitney, Esat Hartford, USA
  Impact of combustor generated temperature distortions on the performance, durability and structural integrity of turbines