The effects of nozzle exit lip thickness on plume resonance

Author:

Ponton M.K.,Seiner J.M.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference15 articles.

1. On the mechanism of choked jet noise;Powell,1953

2. Proposed relationship between broadband shock associated noise and screech tones;Tam;Journal of Sound and Vibration,1986

3. Tones from a choked axisymmetric jet, I: cell structure, eddy velocity and source locations; II: the self excited loop and mode of oscillation;Davies;Acustica,1962

4. The photographic evidence of the feedback loop of a two-dimensional screeching supersonic jet of air;Poldervaart,1968

5. Screech suppression in supersonic jets;Norum;American Institute of Aeronautics and Astronautics Journal,1983

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