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 :

    A numerical analysis applied to high angle of attack three-dimensional inlets


    Contributors:

    Conference:

    Joint Propulsion Conference ; 1986 ; Huntsville, AL, United States


    Publication date :

    1986-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :