Aerodynamic interference between an aircraft and wing store is studied by the use of analytical wing, fuselage, and store models. Inviscid flow is assumed and the Gothert transformation is used to correct for compressibility. An elliptic wing is represented by a bound vortex followed by a trailing vortex sheet. The fuselage and store are assumed to be slender bodies and modeled by a series of sources and doublets along their axis of revolution. Aerodynamic interference of the aircraft model is studied by observing the store in captive and free flight modes in the vicinity of the wing and fuselage models. The aerodynamic forces and moments experienced by the store as well as store trajectories are computed. Comparisons are made of store reactions (motion and trajectory) to only the wing model and to the wing and fuselage models combined. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Interference Between an Aircraft and Wing Store


    Contributors:

    Publication date :

    1973


    Size :

    110 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    NUMERICAL EVALUATION OF AERODYNAMIC INTERFERENCE BETWEEN WING AND FUSELAGE FOR HYPERSONIC EXPERIMENTAL AIRCRAFT

    Tanabe, A. / Matsuo, A. / Kojima, T. et al. | British Library Conference Proceedings | 2010


    Vortex-Lattice-Method to Analyze Aerodynamic Interference of Wing/Pylon/Store Configurations of an F-16 Wing

    Cattarius, J. / Preidikman, S. / Mook, D. T. et al. | British Library Conference Proceedings | 1999



    Wing-Tip-to-Wing-Tip Aerodynamic Interference

    Vlachos, P. / Telionis, D. / AIAA | British Library Conference Proceedings | 2003


    Wing-Tip-To-Wing-Tip Aerodynamic Interference

    Vlachos, Pavlos / Telioinis, Demetri | AIAA | 2003