A state-of-the-art finite difference boundary-layer program incorporated into the NYU Transonic Analysis Program is described. Some possible treatments for the trailing edge region were investigated. Findings indicate the trailing edge region, still within the scope of an iterative potential flow, boundary layer program, appears feasible.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Generalization of Analytical Tools for Helicopter-Rotor Airfoils


    Contributors:
    E. H. Gibbs (author)

    Publication date :

    1979


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Robust aerodynamic optimization of morphing airfoils for helicopter rotor blades

    Fusi, Francesca / Quaranta, Giuseppe / Guardone, Alberto et al. | AIAA | 2015



    Effects of Ballistic Damage on the Aerodynamics of Helicopter Rotor Airfoils

    Keith W. Robinson / J. Gordon Leishman | AIAA | 1998