Numerical and Experimental Studies on Supersonic Free Jet with Various Cross-Sectional Tab Configuration
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-5752-1_61
Reference14 articles.
1. Pack DC (1948) On the formation of shock-waves in supersonic gas jets: two-dimensional flow. Quart J Mech Appl Math 1(1):1–17
2. Love ES, Grigsby E, Lee LP, Woodling MJ (1959) Experimental and theoretical studies of axisymmetric free jets. NASA TR R-6
3. Powell A (1953) On the mechanism of choked jet noise. Proc Phys Soc Sect B 66:1039–1056. https://doi.org/10.1088/0370-1301/66/12/306
4. Umeda Y, Ishii R (2001) On the sound sources of screech tones radiated from choked circular jets. J Acoust Soc Am 110:1845–1858. https://doi.org/10.1121/1.1402620
5. Bradbury LJS, Khadem AH (1975) The distortion of a jet by tabs. J Fluid Mech 70:801. https://doi.org/10.1017/S0022112075002352
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