Small disturbances and aeroelastic effects simulated. XTRAN2L computer program used to calculate two-dimensional transonic flows about airfoils. Uses time-accurate, alternating-direction, implicit (ADI) finite-difference scheme to solve two-dimensional complete unsteady transonic small-disturbance equation. Engquist-Osher monotone spatial differencing used in ADI solution algorithm to provide robust and efficient program. Written in FORTRAN V.


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    Title :

    Calculating Transonic Flows About Airfoils


    Contributors:

    Published in:

    Publication date :

    1989-09-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Perturbation Method for Transonic Flows about Oscillating Airfoils

    R.M. Traci / E.D.Albano / J.L. Farr | AIAA | 1976



    Transonic flow about airfoils

    Bauer, F. / Garabedian, P. / Jameson, A. et al. | NTRS | 1978