Design of S-Shaped Submerged Inlet
2011 ◽
Vol 291-294
◽
pp. 349-354
Keyword(s):
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%.
2012 ◽
Vol 246-247
◽
pp. 446-450
2013 ◽
Vol 444-445
◽
pp. 1345-1349
2021 ◽
pp. 095441002110113
2021 ◽
pp. 095441002098398
2021 ◽
pp. 095441002110295
2003 ◽
Vol 217
(1)
◽
pp. 29-41
◽