By A. Strang, William M. Banks, R. D. Conroy, M. J. Goulette
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2. 3. 4. 5. 6. 7. 8. 9. HALLER, WALKER, SINGH, and INCE: 'Application of 3D computational Fluid Dynamics Methods for enhanced efficiency blading', Fourth International Charles Parsons Turbine Conference, The Institute of Materials, London, November 1997. E Seminar, Latest Advances in the Aerodynamics of turbomachinery with special emphasis upon unsteady flows. December 1996. SINGH,WALKERand HALLER:'Development of three-dimensional stage viscous time marching for optimization of short height stages', First European Conference on Turbomachinery-Fluid dynamic and thermodynamic aspects, Erlangen March 1995, Published in VDr Berichte 1185.
E. % Xl2CrMoVNbN 101, (COST Steel F), for rotor forgings and G-XI2CrMoVNbN 9 1, (modified 9% CrMo steel) for large castings The choice of these two particular variants does not affect the content of the paper and the same conclusions would have been reached if any of the other accepted variants had been chosen. No new material development was required for bolting and blading. High Cr materials are standard and Nimonic 80A is a well established material that provides substantial increase in high temperature properties if required.
In the last stage of blading, exit losses should be minimised. For zero exit swirl, stage reaction and stage loading are related through (7) The aerodynamic design of blading is always constrained by the mechanical strength of the blades. For stator blades, an approximate expression for the bending stresses in terms of ip, 'lj; and R is I _ oi = , 2h' 2 , Ps u t 4W'1,2 fi'lj; V cp 2 + ( 1-R )2 (8) , and for rotor blades, bending and centrifugal stresses are obtained as « (J" "2h"2 >» 4 W"I" 2 b - t" I" 'lj; V 2+ cp 2 Rand (J" "_,,,,2 c - Kp h 2 D" m U , (9) respectively.
Advances in turbine materials, design and manufacturing by A. Strang, William M. Banks, R. D. Conroy, M. J. Goulette
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