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    Numerical study of multi-element airfoil aerodynamics (1992)
    In:  Other Sources
    Details
    Publication Date: 2019-08-27
    Description: Unsteady flowfields around oscillating Boeing VR7 airfoil with and without a leading-edge slat were numerically investigated by a novel zonal method using a conformal mapping technique. Numerical aero-dynamic hysteresis loops show that the leading-edge slat prevents the airfoil dynamic stall at reduced frequency of 0.15, Reynolds number of 1 million, and the oscillation range of 5 deg to 25 deg.
    Keywords: AERODYNAMICS
    Type: ; : Algorithmic trends
    Format: text
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