Experimental verification of the theory describing arbitrary motions of an airfoil is reported. The experimental apparatus is described. A mechanism was designed to provide two separate degrees of freedom without friction or backlash to mask the small but important aerodynamic effects of interest.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Elastic suspension of a wind tunnel test section


    Contributors:
    Hacker, R. (author) / Rock, S. (author) / Debra, D. B. (author)


    Publication date :

    1982-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Wind Tunnel Test Section Patent Application

    J. W. Davis / O. E. Hill | NTIS | 1969


    Rigid-elastic coupling flutter wind tunnel test device

    ZHANG GENGGENG / PU LIDONG / LI JUNJIE et al. | European Patent Office | 2024

    Free access