The separated flow method is evaluated. This method was developed for moderately swept wings with multiple, constant strength vortex systems. The flow on the highly swept wing used in this evaluation is characterized by a single vortex system of continuously varying strength.


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    Title :

    Aeroelastic Loads Prediction for an Arrow Wing. Task 1: Evaluation of R. P. White's Method


    Contributors:
    C. J. Borland (author) / M. E. Manro (author)

    Publication date :

    1983


    Size :

    93 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English