Multiple metrics are applied to the design of a large civil tiltrotor, integrating minimum cost and minimum environmental impact. The design mission is passenger transport with similar range and capacity to a regional jet. Separate aircraft designs are generated for minimum empty weight, fuel burn, and environmental impact. A metric specifically developed for the design of aircraft is employed to evaluate emissions. The designs are generated using the NDARC rotorcraft sizing code, and rotor analysis is performed with the CAMRAD II aeromechanics code. Design and mission parameters such as wing loading, disk loading, and cruise altitude are varied to minimize both cost and environmental impact metrics. This paper presents the results of these parametric sweeps as well as the final aircraft designs.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Application of Climate Impact Metrics to Civil Tiltrotor Design


    Beteiligte:
    C. R. Russell (Autor:in) / W. Johnson (Autor:in)

    Erscheinungsdatum :

    2013


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Application of Climate Impact Metrics to Civil Tiltrotor Design

    Russell, C. / Johnson, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013


    Application of Climate Impact Metrics to Civil Tiltrotor Design

    Russell, Carl R. / Johnson, Wayne | NTRS | 2013


    Application of Climate Impact Metrics to Civil Tiltrotor Design

    Russell, Carl / Johnson, Wayne | AIAA | 2013


    Civil Tiltrotor Aircraft Operations

    Young, L. / Chung, W. / Paris, A. et al. | British Library Conference Proceedings | 2011


    Short Haul Civil Tiltrotor

    SAE / American Helicopter Society / AIAA | British Library Conference Proceedings | 1997