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Effect of Fan on Inlet Distortion: Mixed-fidelity Approach
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 Reynolds-averaged Navier–Stokes or unsteady Reynolds-averaged Navier–Stokes to model this unsteady interaction, due to the substantialdoi:10.17863/cam.23422 fatcat:x5okbuxv4bawlm4qaojounimqi