NASA NTRS · 19860058022
A numerical analysis applied to high angle of attack three-dimensional inlets
Abstract
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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Hwang, D. P.. 1986-06-01. A numerical analysis applied to high angle of attack three-dimensional inlets. https://ntrs.nasa.gov/citations/19860058022
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