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.
A numerical analysis applied to high angle of attack three-dimensional inlets
Joint Propulsion Conference ; 1986 ; Huntsville, AL, United States
1986-01-01
Conference paper
No indication
English