CUED Publications database

Effect of Fan on Inlet Distortion: A Mixed-fidelity Approach

Ma, Y and Cui, J and Vadlamani, N and Tucker, P Effect of Fan on Inlet Distortion: A Mixed-fidelity Approach. AIAA Journal. (Unpublished)

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Abstract

Inlet distortion is typically encountered during off-design conditions on civil aircraft and in S-ducts in military aircraft. It is known to cause severe deterioration to the performance of a gas-turbine engine. As intakes become shorter, there is an increased interaction between the inlet distortion and the downstream fan. Previous studies in the literature use RANS or URANS to model this unsteady interaction, due to the substantial computational cost associated with high-fidelity methods such as LES/DNS. On the other hand, it is well known that turbulence models have limitations in terms of predicting distorted flows. In this paper, we propose a mixed-fidelity approach and employ it to study the intake-fan interaction at an affordable computational cost. The results demonstrate that there are two mechanisms via which the fan affects the separated flow. Firstly, the suction effect of the fan (effective up to almost half of the chord length upstream of the fan) alleviates the undesired distortion by ‘directly’ changing the streamline curvature, intensifying the turbulence transport and closing the recirculation bubble at a much earlier point in time. Secondly, the enhanced turbulence in the vicinity of the fan feeds back into the initial growth of the shear layer by means of the recirculating flow. This ‘indirect’ feedback is found to increase turbulence production during the initial stages of formation of the shear layer. Both the direct and indirect effects of the fan significantly suppress the inlet distortion.

Item Type: Article
Subjects: UNSPECIFIED
Divisions: Div A > Fluid Mechanics
Div A > Turbomachinery
Depositing User: Cron Job
Date Deposited: 08 Mar 2018 01:25
Last Modified: 19 Jul 2018 07:09
DOI: