IMECH-IR  > 高温气体动力学国家重点实验室
Analysis of the test condition of a shock-expansion tube: JF-16
Hu ZM(胡宗民); Wu B(吴波); Jiang ZL(姜宗林)
Source PublicationProceedings of the First International Conference on High Temperature Gas Dynamics
2012-10
Conference NameFirst International Conference on High Temperature Gas Dynamics
Conference Date2012-10
Conference PlaceBeijing
AbstractA shock-expansion tube (SET, named JF-16) has been built at the State Key Laboratory of High Temperature Gas Dynamics (LHD) in order to generate relatively steady and clean test gas of really high enthalpy. However, the test time of a SET is extremely shorter as compared to a reflected-shock tunnel (RST) of the same scale which results in difficulties in the measurements and diagnostics. An applicable means to the flow diagnostics is the integrated computation-experiment techniques. In this paper, some numerical issues occurring in our computational investigation for the test flow of JF-16 are discussed. The dispersion-controlled dissipative scheme (DCD) is used to setup our SET simulation code. However, spurious oscillation at the contact surface occurs when the original scheme is applied to the simulation of JF-16 test flow. A new flux splitting algorithm based on local characteristics is worked out for the DCD scheme. Preliminary computations indicate that the updated algorithm is more robust to suppress the aforementioned oscillation as compared to the original algorithm. Several experiments with the typical hypervelocity test flow of JP-16 are computed and compared to validate the algorithms. The computations of double-wedge flows indicate that the experimental visualization is mainly the self-illumination of nitrogen atoms instead of the schlieren image.
KeywordShock-expansion Tube Computation Spurious Oscillation Flus Splliting
DepartmentLHD激波与爆轰物理
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/47093
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
Hu ZM,Wu B,Jiang ZL. Analysis of the test condition of a shock-expansion tube: JF-16[C],2012.
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