A summary of participants’ results for the coupled aerostructural simulation test case from the Sixth AIAA Computational Fluid Dynamics Drag Prediction Workshop held in Washington, DC, 16–17 June 2016, is presented. The test case focuses on a static aeroelastic simulation of NASA’s Common Research Model civil transport aircraft in the wing/body configuration (i.e., without engines, pylons, and empennage). Flow conditions include the design point lift coefficient C L = 0.5 ± 0.0001 at cruise flight. Aeroelastic simulations are performed on the “medium” baseline grid, coupled to a computational structural analysis, using either an existing finite element model or modal data. Experimental validation data for this test case are available from a wind-tunnel test campaign performed at the European Transonic Wind Tunnel in Cologne, Germany.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Summary of Case 5 from Sixth Drag Prediction Workshop: Coupled Aerostructural Simulation


    Beteiligte:
    Keye, Stefan (Autor:in) / Mavriplis, Dimitri (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 55 , 4 ; 1380-1387


    Erscheinungsdatum :

    01.07.2018




    Medientyp :

    Aufsatz (Konferenz) , Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Summary Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases

    Tinoco, Edward N. / Brodersen, Olaf P. / Keye, Stefan et al. | AIAA | 2018

    Freier Zugriff


    Summary Data from the Sixth AIAA Computational Fluid Dynamics Drag Prediction Workshop: Code Verification

    Roy, Christopher J. / Rumsey, Christopher L. / Tinoco, Edward N. | AIAA | 2018