Methodology assessment for the design and analysis of aero-engine short intakes

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dc.contributor.author Boscagli, Luca
dc.contributor.author Christie, Robert
dc.contributor.author MacManus, David G.
dc.date.accessioned 2020-10-13T15:02:13Z
dc.date.available 2020-10-13T15:02:13Z
dc.date.issued 2020-02-28
dc.identifier.citation Boscagli L, Christie R, MacManus DG. (2020) Methodology assessment for the design and analysis of aero-engine short intakes. In: Aerospace Europe Conference 2020 (AEC2020) 25-28 February 2020, Bordeaux, France en_UK
dc.identifier.uri https://www.cleansky.eu/event/aerospace-europe-conference-eac2020
dc.identifier.uri https://dspace.lib.cranfield.ac.uk/handle/1826/15880
dc.description.abstract A key aspect for the design of an aero-engine intake is that it must operate at off-design conditions such as high incidence. For short intake design the interaction with the fan cannot be neglected. This work establishes how different modelling strategies can affect the intake design boundaries and the analysis of an aero-engine short-intake. Unsteady simulations showed high levels of total pressure and swirl fluctuations while steady computations showed some limitations whenever extreme operating conditions are modelled. The analysis of a short intake showed that the fan is able to extend the incidence limit to avoid separation by about 0.6°. Overall, this work proposes a robust methodology for short-intake analysis en_UK
dc.language.iso en en_UK
dc.publisher CEAS en_UK
dc.rights Attribution-NonCommercial 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by-nc/4.0/ *
dc.subject unsteady en_UK
dc.subject flow distortions en_UK
dc.subject fan coupling en_UK
dc.subject short intake en_UK
dc.title Methodology assessment for the design and analysis of aero-engine short intakes en_UK
dc.type Conference paper en_UK


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