The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed. Based on the loitering aircraft, a s-shaped inlet was designed to meet the needs of stable flight of loitering aircraft, whose total pressure recovery coefficient is 93.2% and total pressure distortion coefficient is 1.2%.
Design of S-Shaped Submerged Inlet
Advanced Materials Research ; 291-294 ; 349-354
04.07.2011
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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