With reference to problem of rotating compressor stall, unsteady boundary layer calculation is made to find unsteady increment of lift of stalled elliptic airfoil in flow of time dependent incidence.


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    Title :

    Lift hysteresis at stall as unsteady boundary-layer phenomenon


    Additional title:

    NACA -- Tech Note


    Contributors:
    Moore, F.K. (author)


    Publication date :

    1955


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English








    Unsteady Flow Simulation of High-Lift Stall Hysteresis Using a Lattice Boltzmann Approach

    Fares, E. / Fabiano, E. / Nolting, S. et al. | British Library Conference Proceedings | 2012