Broadband shock noise reduction in turbulent jets by water injection

Author:

Kandula Max

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference18 articles.

1. Orderly structure as a source of jet exhaust noise: Survey lecture, structures and mechanisms of turbulence II;Crighton,1977

2. Seiner JM. Advances in high speed jet aeroacoustics; 1984. AIAA-84-2275.

3. Shock-refracted acoustic wave model for screech amplitude in supersonic jets;Kandula;AIAA J,2008

4. Dougherty NS, Guest SH. A correlation of scale model and flight aeroacoustic data for the Space Shuttle vehicle. In: AIAA/NASA 9th aeroacoustics conference, Williamsburg, Virginia; October 1984. AIAA-84-2351.

5. Jones JH. Scaling of ignition startup pressure transients in rocket systems as applied to the space shuttle overpressure phenomenon. In: JANNAF 13th Plume technology meeting, vol. 1; 1982. CPIA-PUB-357.

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