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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    Title :

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


    Contributors:
    D. P. Hwang (author)

    Publication date :

    1986


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English