This paper describes the results of a Lockheed parametric analysis of the performance, environmental factors, and economics of an advanced commercial transport envisioned for operation in the post-1985 time period. The design parameters investigated include cruise speeds from Mach 0.85 to Mach 1.0, passenger capacities from 200 to 500, ranges of 2800 to 5500 nautical miles, and noise level criteria. NASA high performance configurations and alternate configurations are operated over domestic and international route structures. Indirect and direct costs and return on investment are determined for approximately 40 candidate aircraft configurations. The candidate configurations are input to an aircraft sizing and performance program which includes a subroutine for noise criteria. Comparisons are made between preferred configurations on the basis of maximum return on investment as a function of payload, range, and design cruise speed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Parametric analysis of ATT configurations.


    Beteiligte:
    Lange, R. H. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aircraft Design, Flight Test, and Operations Meeting ; 1972 ; Los Angeles, CA


    Erscheinungsdatum :

    01.08.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Parametric CFD Study for Modified HOPE-X Configurations

    Yamamoto, Y. / Ito, R. | British Library Conference Proceedings | 2000



    Backward parametric interactions in quasi-phase matched configurations

    Aschieri, P. / Baldi, P. / De Micheli, M. P. et al. | British Library Conference Proceedings | 1998