A three-component internal strain-gauge balance for use in a cryogenic wind tunnel has been developed by National Aerospace Laboratory NLR. With this balance model tests were performed in the NASA Langley 0.3-m Transonic Cryogenic Tunnel. The results are discussed with a view to the development of strain-gauge balances for the European Transonic Wind Tunnel (ETW).


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    Titel :

    Development of a Multi-Component Internal Strain-Gauge Balance for Model Tests in a Cryogenic Wind Tunnel


    Beteiligte:
    J. F. Baljeu (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    99 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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