Phugoid motions in compressible range are defined assuming that thrust is equal to drag and moments about aircraft center of gravity equal zero; under these conditions, both incidences for constant elevator settings, and fuel admission are functions of Mach number; elements of motion and equation of path are deduced with respect to incompressible range.


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    Title :

    Phugoid paths of high-speed aircraft


    Additional title:

    Rev de Mecanique Appliquee


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    15 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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