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.
Numerical Analysis Applied to High Angle of Attack Three-Dimensional Inlets
1986
16 pages
Report
Keine Angabe
Englisch