On the generation of entropy noise in a shock containing nozzle of high-performance aircraft at afterburner

Author:

Tam Christopher K.W.

Publisher

Elsevier BV

Subject

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

Reference55 articles.

1. Similarity spectra analysis of high-performance jet aircraft noise;Neilsen;J. Acoust. Soc. Am.,2013

2. The role of nonlinear effects in the propagation of noise from high-power jet aircraft;Gee;J. Acoust. Soc. Am.,2008

3. Near-field noise measurements of a high-performance military jet aircraft;Wall;Noise Control Eng,2012

4. Spectral Characterization in the Near-and Mid-Field of Military Jet Aircraft Noise;Neilsen,2013

5. Noise of high-performance aircraft at afterburner;Tam;J. Sound Vib.,2015

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1. On a New Jet Noise Component From High-Performance Aircraft at Afterburner;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Preliminary design and analysis of an afterburner module;International Journal of Aeronautics and Astronautics;2023-12-31

3. Jet Noise Reduction: A Fresh Start;AIAA AVIATION 2023 Forum;2023-06-08

4. Contoured Insert Jet Noise Reduction Concept Applied to a Lab-Scale Representation of an Afterburning Supersonic Jet;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

5. Supersonic jet noise source distributions;The Journal of the Acoustical Society of America;2021-09

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