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EPSRC Reference: GR/M43821/01
Title: COMPUTATION OF UNSTEADY FLOW AROUND OSCILLATING BLADES IN MULTIPLE BLADEROWS BY A SINGLE-PASSAGE APPROACH
Principal Investigator: He, Professor L
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Department: Engineering and Computing Sciences
Organisation: Durham, University of
Scheme: Standard Research (Pre-FEC)
Starts: 01 July 1999 Ends: 30 June 2002 Value (£): 155,198
EPSRC Research Topic Classifications:
Aerodynamics
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
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Summary on Grant Application Form
Understanding and prediction of unsteady flow effects are important in development of modern high performance turbomachinery. Conventional multi-passage time-domain CFD calculations are featured by very high demands on computing resources. For blade flutter applications, unsteady flow computations for oscillating blades would normally have to be carried out for a whole annulus configuration. This would be extremely time-consuming, even for an isolated bladerow. It has been recently shown that adjacent bladerows can have profound effects on blade aeroelastic stability. The need to include the multi-bladerow effects in blade flutter analysis presents a further challenge to the conventional multi-passage approach.It is proposed to develop, validate and apply an efficient single-passage approach to unsteady flow computations. The approach will be based on a novel Fourier-tranform based phase-shift periodic condition method, capable of dealing with multiple unsteady disturbances. It will be implemented in a 3D time-marching Navier-Stokes solver. The validity and effectiveness of the new method will be examined and demonstrated in comparison with the conventional multi-passage approach. The method will be applied to analysing aeroelastic characteristics of a rotor bladerow embedded in multiple bladrows. The work will be carried out by a postdoctoral research assistant with intensive use of a modern workstation.
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