TY - GEN
T1 - Design of s-shaped submerged inlet
AU - He, Guanglin
AU - Li, Xiaolin
PY - 2011
Y1 - 2011
N2 - 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%.
AB - 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%.
KW - Distortion coefficient
KW - Loitering aircraft
KW - Recovery coefficient
KW - S-shaped inlet
UR - https://www.scopus.com/pages/publications/79961202094
U2 - 10.4028/www.scientific.net/AMR.291-294.349
DO - 10.4028/www.scientific.net/AMR.291-294.349
M3 - Conference contribution
AN - SCOPUS:79961202094
SN - 9783037851937
T3 - Advanced Materials Research
SP - 349
EP - 354
BT - Materials Processing Technology
T2 - 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011
Y2 - 29 July 2011 through 31 July 2011
ER -