Review of theoretical work done at Royal Aircraft Establishment, which was limited to case of zero incidence; results do not depend on lift theories, and belong entirely to field of classical hydrodynamics; method used is that of sources and sinks and is really linear perturbation theory for thin airfoils.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Critical mach numbers for swept-back wings


    Additional title:

    Aeronautical Quarterly


    Contributors:
    Neumark, S. (author)

    Published in:

    Publication date :

    1950


    Size :

    26 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Critical Mach Number Prediction on Swept Wings

    Kirkman, Jeffrey J. / Takahashi, Timothy T. | AIAA | 2017


    Critical Mach Number Prediction on Swept Wings (AIAA 2017-0266)

    Kirkman, Jeffrey J. / Takahashi, Timothy T. | British Library Conference Proceedings | 2017