A winged aerothermodynamic experimental reentry vehicle is proposed in order to verify and validate the methods of numerical aerothermodynamics as design tool additional to the classical tools, i.e., the wind tunnel. Experimental hypersonic vehicles are reviewed and the aerothermodynamic characteristic of reentry vehicles and the ground simulation problems are considered. The possible configuration and trajectory of a winged experimental vehicle are discussed, together with the required and possible measurements, and the data management and recovery. Use of the obtained data base in the establishment of the methods of numerical aerothermodynamics as additional design tool is outlined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Acquisition of an Aerothermodynamic Data Base by Means of a Winged Experimental Reentry Vehicle


    Beteiligte:
    E. H. Hirschel (Autor:in) / H. Grallert (Autor:in) / J. Lafon (Autor:in) / M. Rapuc (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    40 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Acquisition of an aerothermodynamic data base by means of a winged experimental reentry vehicle

    Hirschel, E.H. / Grallert, H. / Lafon, J. et al. | Tema Archiv | 1992


    Acquisition of an aerothermodynamic data base by means of a winged experimental reentry vehicle

    Hubschrauber und Flugzeuge, Messerschmitt-Bölkow-Blohm GmbH, Ottobrunn | TIBKAT | 1991



    Aerothermodynamic Reentry Flight Experiments Expert

    Muylaert, J. / Walpot, L. / Ottens, H. et al. | British Library Conference Proceedings | 2007