The three-dimensional analytical methods used to analyze subsonic high angle of attack inlets are described. The methods are shown to be in good agreement with experimental results for various three-dimensional high angle of attack inlets. The methods are used to predict aerodynamic characteristics of scarf and slotted-lip inlets.


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    Titel :

    Numerical Analysis Applied to High Angle of Attack Three-Dimensional Inlets


    Beteiligte:
    D. P. Hwang (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch