Boundary layer method for unsteady aerodynamic loads determination

2010 
In this work a simple and accurate method for two-dimensional unsteady aerodynamic load determination on airfoil is developed. The method employs visc
    • Correction
    • Source
    • Cite
    • Save
    • Machine Reading By IdeaReader
    0
    References
    1
    Citations
    NaN
    KQI
    []