Studies of a Caret Inlet at Subsonic Speeds

[1] Hall G R, Hurwitz W M, Tiebens G S, et al. Development of the F/A-18 E/F air induction system. AIAA 93-2152, 1993 [2] 何志强,郭荣伟. 双斜切双压缩面进气道进口波系结构的数值研究[J]. 航空学报, 1999, 20(4):339~342 He Zhiqiang, Guo Rongwei. Numerical investigation of shockwaves at the entrance of dual-swept/dual-ramp inlet[J]. Acta Aeronautica et Astronautica Ainica, 1999, 20(4):339~342(in Chinese) [3] Philhower J S, Robinson D E, Brown R J. Development of a highly offset induction system for a supersonic STOVL fighter. AIAA 98-3417, 1998 [4] 钟易成,余少志,陈 晓. 低速来流大攻角侧滑角状态下尖脊进气道气动特性试验研究[J]. 航空动力学报,2001,16(1):23~ 27 Zhong Yicheng, Yu Shaozhi, Chen Xiao. Experimental investigation on gas-dynamic performance of caret inlet under condition of large attack angles and yaw angles[J]. Journal of Aerospace Power, 2001,16(1):23~27(in Chinese) [5] 朱 宇,李椿萱,李 天.后掠压缩面进气道激波特性数值研究[J].飞机设计,2001(4):1~5 Zhu Yu, Li Chunxuan, Li Tian. Study of supersonic flow field characteristics at the entrance of dual-swept/dual-ramp inlet[J]. Plane Design, 2001(4):1~5(in Chinese) [6] 谭慧俊,郭荣伟.一种双斜切双压缩面进气道性能的数值模拟[J].空气动力学学报,2001,19(3):338~343 Tan Huijun, Guo Rongwei.Numerical simulation of a dual-swept/dual/ramp inlet. Acta Aerodynamica Sinica, 2001,19(3):338~343(in Chinese) [7] Jameson A, Schmidt W, Turkel E. Numerical solution of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes. AIAA 81-1259, 1981 [8] Barth T J, Jespersen D. The design and application of upwind schemes on unstructured meshes. AIAA 89-0366, 1989 [9] Jones W P, Launder B E. The prediction of laminarization with a two equation model of turbulence[J]. International Journal of Heat and Mass Transfer,1972, 15:301~314 [10] Launder B E, Spalding D B. The numerical computation of turbulent flows[J]. Computer Methods in Applied Mechanics and Engineering,1974,3:269~289