Problems involved in airplane icing at high altitudes and in freezing, stiffening, and failure of variety of mechanical rubber articles used in airplane construction, have necessitated use by large manufacturing companies of freezing chambers for testing, development, and research work; description of low temperature chamber designed by Heinkel Aeroplane Co, suitable for smallest scale laboratory operations; principle used is that of freezing in air current in what is really low speed tunnel. English translation from Kunststoffe v 33 1943 p 107.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Laboratory "Wind-Tunnel"


    Additional title:

    India-Rubber J


    Published in:

    Publication date :

    1944


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Avionics wind tunnel laboratory interface development

    Howell, D. / Woodyard, J. / Wiseman, J. et al. | IEEE | 1993



    Propulsion wind tunnel at naca lewis laboratory

    Wasielewski, E. W. | NTRS | 1956


    Pressure Sensitive Paints: from Laboratory to Wind Tunnel

    Mebarki, Y. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2000