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
01.01.1986
Aufsatz (Konferenz)
Keine Angabe
Englisch