Scaling Laws at Stall in an Axial Compressor with an Upstream Perturbation
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DOI: 10.2514/1.b39407
Abstract: An experimental campaign has been conducted to assess the effect of total pressure inlet distortion on a single stage axial compressor. Different grid sectors have been installed in front of the inlet of the compressor… read more here.
Keywords: axial compressor; scaling laws; flow regimes; laws stall ... See more keywords