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タイトルBackground Oriented Schlieren Applied to Study Shock Spacing in a Screeching Circular Jet
本文(外部サイト)http://hdl.handle.net/2060/20120003980
著者(英)Zaman, Khairul B. M. Q.; Fagan, Amy F.; Clem, Michelle M.
著者所属(英)NASA Glenn Research Center
発行日2012-01-09
言語eng
内容記述Background oriented schlieren (BOS) is a recent development of the schlieren and shadowgraph methods. The BOS technique has the ability to provide visualizations of the density gradient in both the axial and radial directions. The resultant magnitude of the density gradients allows for comparison with shadowgraph images. This paper first compares data obtained by the BOS and shadowgraph techniques at identical conditions in a free jet. The patterns and spacing of the shock trains obtained by the two techniques are found to be consistent with one another. This provides confidence in the shock spacing measurement by the BOS technique. Due to its simpler setup, BOS is then applied to investigate the shock spacing associated with the screech phenomenon, especially during stage jumps. Screech frequencies from a 37.6 mm convergent nozzle, as a function of jet Mach number (M(sub j)), are shown to exhibit various stages. As many as eight stages are identified with the present nozzle over the range 1.0 < M(sub j) <1.7. BOS images are acquired at various screech conditions and the shock spacing is examined as a function of M(sub j).
NASA分類Fluid Mechanics and Thermodynamics
レポートNOE-18135
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/243284


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