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    Development of a nonlinear switching function and its application to static lift characteristics of straight wings (1978)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A mathematical modeling technique was developed for the lift characteristics of straight wings throughout a very wide angle of attack range. The technique employs a mathematical switching function that facilitates the representation of the nonlinear aerodynamic characteristics in the partially and fully stalled regions and permits matching empirical data within + or - 4 percent of maximum values. Although specifically developed for use in modeling the lift characteristics, the technique appears to have other applications in both aerodynamic and nonaerodynamic fields.
    Keywords: AERODYNAMICS
    Type: NASA-TM-78737 , L-12270
    Format: application/pdf
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