The deformable leading edge (DLE) concept to improve the blade capability in lift, drag and pitching moments has been investigated for the purpose of meeting new rotor maneuverability and susceptibility requirements. The advantages and disadvantages of this concept have been carefully examined with limited computational and experimental results. This work showed that this concept achieves a substantial improvement in lift capability and also reduces the drag and pitching moment at the same time. Effects of various parameters, such as Reynolds number, reduced frequency, mean angle of oscillation, and airfoil shape, on the performance of these airfoils were also investigated.


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    Titel :

    Characteristics of deformable leading edge for high performance helicopter rotor


    Beteiligte:
    Lee, Soogab (Autor:in) / Mcalister, K. W. (Autor:in) / Tung, Chee (Autor:in)


    Erscheinungsdatum :

    1993-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Characteristics of deformable leading edge for high performance helicopter rotor

    LEE, SOOGAB / MCALISTER, K. / TUNG, CHEE | AIAA | 1993


    Characteristics of Deformable Leading-Edge for High-Performance Helicopter Rotor

    Lee, S. / McAlister, K. / Tung, C. et al. | British Library Conference Proceedings | 1993


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    Colpitts, Robert R. / Nayman, Maurice / Perez, Ruben E. | TIBKAT | 2021


    Optimization of Leading Edge Tubercles Applied to Helicopter Rotor Blades

    Colpitts, Robert R. / Nayman, Maurice / Perez, Ruben E. | AIAA | 2021


    Deformable Leading Edge Electromechanical Airfoil

    Fink, D. A. / Reinhardt, N. / Severance, R. et al. | British Library Conference Proceedings | 2007