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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    Title :

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


    Contributors:

    Publication date :

    1988


    Size :

    99 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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