Effect of a tab on the aerodynamical development and noise of an underexpanded supersonic jet

Author:

André Benoît,Castelain Thomas,Bailly Christophe

Publisher

Elsevier BV

Subject

Mechanics of Materials,General Materials Science

Reference26 articles.

1. Measurement of shock structure and shock–vortex interaction in underexpanded jets using Rayleigh scattering;Panda;Phys. Fluids,1999

2. On the mechanism of choked jet noise;Powell;Proc. Phys. Soc. B,1953

3. Proposed relationship between broadband shock associated noise and screech tones;Tam;J. Sound Vib.,1986

4. Noise associated with shock waves in supersonic jets;Martlew;AGARD CP,1969

5. The noise from shock waves in supersonic jets;Harper-Bourne;AGARD CP,1973

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4. Computational Investigation of Jet Mixing Enhancement by C-D Nozzle using Triangular Tabs;2022 International Conference on Power, Energy, Control and Transmission Systems (ICPECTS);2022-12-08

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