Equations and charts have been presented for the conical part of the sidewash above and below swept wings at small angles of attack. This flow-field component is necessary in making calculations of the wing-induced forces and moments on stores, missiles, and pylons. All supersonic Mach numbers and wing leading-edge sweep angles have been considered.


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    Titel :

    Sidewash in the Vicinity of Lifting Swept Wings at Supersonic Speeds


    Beteiligte:

    Erscheinungsdatum :

    1957-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch