Studies on the starting transient of a straight cylindrical supersonic exhaust diffuser: Effects of diffuser length and pre-evacuation state

被引:23
|
作者
Park, Byung Hoon [1 ]
Lee, Ji Hyung [1 ]
Yoon, Woongsup [1 ]
机构
[1] Yonsei Univ, Prop & Environm Thermofluids Lab, Sch Mech Engn, Seoul 120749, South Korea
关键词
Supersonic exhaust diffuser (SED); High altitude test (HAT); Starting transient; Short diffuser; Diffuser mode-transition;
D O I
10.1016/j.ijheatfluidflow.2008.04.006
中图分类号
O414.1 [热力学];
学科分类号
摘要
Effects of essential performance parameters on the starting transient of a straight cylindrical supersonic exhaust diffuser (SED) are numerically investigated. Diffuser starting and evacuation transients are examined in terms of SED lengths and pre-evacuation configuration. Preconditioned Favre-averaged Navier-Stokes equations incorporated with a low Reynolds number turbulence model and Sakar's method to treat turbulence compressibility is solved for strongly turbulent all-Mach diffuser flows. The numerical method is properly validated with the measurements with accuracy. Characteristic locus of diffuser-starting and diffuser-unstarting modes is constructed for the diffusers of three different lengths (L/D = 2, 5, and 20). Flow evolutions visualized in diffuser mode-transition regimes manifest a threshold L/D over which the SED starting transient is unique. An occurrence of plume blowback into the vacuum chamber due to lower initial pressure (P-C.INIT/P-A = 0.0027) expedites expansion of nozzle exhaust and diffuser choking, and causes faster chamber evacuation than the atmospheric starting. (C) 2008 Elsevier Inc. All rights reserved.
引用
收藏
页码:1369 / 1379
页数:11
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