Details
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
Additional Information
Manufacturer | von Karman Institute for Fluid Dynamics |
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