Studies of transport aircraft designed for boom-free supersonic flight show the variable sweep oblique wing to be the most efficient configuration for flight at low supersonic speeds. Use of this concept leads to a configuration that is lighter, quieter, and more fuel efficient than symmetric aircraft designed for the same mission. Aerodynamic structural, weight, aeroelastic and flight control studies show the oblique wing concept to be technically feasible. Investigations are reported for wing planform and thickness, pivot design and weight estimation, engine cycle (bypass ratio), and climb, descent and reserve fuel. Results are incorporated into a final configuration. Performance, weight, and balance characteristics are evaluated. Flight control requirements are reviewed, and areas in which further research is needed are identified.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Oblique wing transonic transport configuration development


    Erscheinungsdatum :

    1977-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Transonic Wind-Tunnel Test Of An Oblique Wing

    Kennelly, R. A. / Strong, J. M. / Carmichael, R. L. et al. | NTRS | 1992


    Transonic transport wings - Oblique or swept

    Jones, R. T. / Nisbet, J. W. | NTRS | 1974


    Transonic transport wings - Oblique or swept

    Jones, R. T. / Nisbet, J. W. | NTRS | 1974