The parameters of training jets are usually at the lower limit of the transonic region. The aeroelastic phenomena which are observed are considerably influenced by air compressibility. The theoretical solution of these phenomena does not yield satisfactory results, and there is a need for the use of model systems. This contribution analyzes the capabilities of aeroelastic modelling by a transonic model.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Some Problems of Modelling Aeroelastic Phenomena in a Transonic Tunnel


    Beteiligte:
    J. Malecek (Autor:in) / J. Vrhel (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Conjectures on New Transonic Aeroelastic Phenomena

    Anderson, J. | British Library Conference Proceedings | 1995


    Aeroelastic Studies Using Transonic Flow CFD Modelling

    Badcock, K. / Sim, G. / Richards, B. | British Library Conference Proceedings | 1995


    Rotorcraft aeroelastic testing in the Langley Transonic Dynamics Tunnel

    Yeager, W.T. jun. / Mirick, P.H. / M-Nabil H. Hamouda et al. | Tema Archiv | 1993


    Multiscale Mesh Adaptation for Transonic Aeroelastic Flutter Problems

    Jacobson, Kevin / Stanford, Bret / Kiviaho, Jan F. et al. | AIAA | 2021


    Recent rotorcraft aeroelastic testing in the Langley Transonic Dynamics Tunnel

    Yeager, William T., Jr. / Mirick, Paul H. / Wilbur, Matthew L. et al. | NTRS | 1991