33th Congress of the International Council of the Aeronautical Sciences

03.4 - Applied Aerodynamics

A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET

P. Yan, Shenyang Aircraft Design and Research Institute, China; F. Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China

To improve the performance of submerged inlet, a novel submerged inlet is designed based on the integration design concept of fuselage and inlet. The performance is obtained by numerical simulation and the results indicate that changing the shape curvature of the fuselage can increase the performance of the inlet.


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