On loading corrections and loss distributions in low-speed forward swept axial compressor rotors

Loading of a swept aerofoil blade is typically reduced as its lifting line is inclined (at the sweep angle) with the radial direction. Various estimations are available in the literature about the correction to be made on the loading of a wing when the same is swept. However, it is difficult to obta...

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Veröffentlicht in:Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy Journal of power and energy, 2011-02, Vol.225 (1), p.120-130
Hauptverfasser: Ramakrishna, P V, Govardhan, M
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Sprache:eng
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