The design of modern aircraft requires the solution of problems related to transonic flow at high Reynolds numbers. To investigate these problems experimentally, it is proposed to extend the Ludwieg tube facility in Gottingen by adding a transonic cryogenic test section. After stating the requirements for such a test section, the technical concept is briefly explained and a preliminary estimate of concept is briefly explained and a preliminary estimate of the costs is given.


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    Titel :

    Transonic Cryogenic Test Section for the Goettingen Tube Facility


    Beteiligte:
    H. Hornung (Autor:in) / G. Hefer (Autor:in) / P. Krogmann (Autor:in) / E. Stanewsky (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Transonic cryogenic test section for the Goettingen tube facility

    Hornung, H. / Hefer, G. / Krogmann, P. et al. | NTRS | 1983


    Transonic Cryogenic Test Section for the Goettingen Tube Facility

    H. Hornung / G. Hefer / P. Krogmann et al. | NTIS | 1983




    Cryogenic Balance Technology at the National Transonic Facility (Invited)

    Parker, P. A. / AIAA | British Library Conference Proceedings | 2001