The underexpanded jet Mach disk and its associated shear layer

被引:77
作者
Edgington-Mitchell, Daniel [1 ]
Honnery, Damon R. [1 ]
Soria, Julio [1 ,2 ]
机构
[1] Monash Univ, Lab Turbulence Res Aerosp & Combust, Clayton, Vic 3800, Australia
[2] King Abdulaziz Univ, Dept Aeronaut Engn, Jeddah 21413, Saudi Arabia
基金
澳大利亚研究理事会;
关键词
FRAME RATE SCHLIEREN; COHERENT STRUCTURES; AXISYMMETRICAL JET; SHOCK-REFLECTION; ROCKET NOZZLES; SUPERSONIC JET; TURBULENCE; DYNAMICS; PATTERN; FLOWS;
D O I
10.1063/1.4894741
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
High resolution planar particle image velocimetry is used to measure turbulent quantities in the region downstream of the Mach disk in an axisymmetric underexpanded jet issuing from a convergent nozzle. The internal annular shear layer generated by the slip line emanating from the triple point is shown to persist across multiple shock cells downstream. A triple decomposition based on Proper Orthogonal Decomposition shows that the external helical structure associated with the screech tone generated by the jet exerts a strong influence on velocity fluctuations in the initial region of the annular shear layer. This influence manifests as the external vortices producing oscillatory motion of the Mach disk, and thus a forcing of the internal annular shear layer. The internal shear layer is characterized by a number of azimuthal modes of varying wavenumber and type, including both helical and axisymmetric modes. Finally, the possibility of a previously hypothesized recirculation region behind the Mach disk is investigated, with no evidence found to support its existence. (C) 2014 AIP Publishing LLC.
引用
收藏
页数:18
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