On jet instability modes of a subsonic Hartmann whistle
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/article/10.1007/s12046-018-0921-z/fulltext.html
Reference27 articles.
1. Hartmann J 1922 On a new method for the generation of sound-waves. Phys. Rev. 20(6): 719
2. Raman G and Srinivasan K 2009 The powered resonance tube: from Hartmann’s discovery to current active flow control applications. Prog. Aerosp. Sci. 45(4): 97–123
3. Chang K S, Kim K H and Iwamoto J 1996 A study on the Hartmann–Sprenger tube flow driven by a sonic jet. A study on the Hartmann–Sprenger tube flow driven by a sonic jet 13(3): 173–182
4. Hamed A, Das K and Basu D 2002 Numerical simulation of unsteady flow in resonance tube. AIAA Paper 1118:2002
5. Cain A B, Kerschen E J and Raman G 2002 Simulation of acoustic characteristics and mechanisms of powered resonance tubes. In: Proceedings of the 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO
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