Computation of Large Turbulence Structures and Noise of Supersonic Jets
- Tam, Christopher
- Physical Description:
- 1 electronic document
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- Unclassified, Unlimited, Publicly available.
- Our research effort concentrated on obtaining an understanding of the generation mechanisms and the prediction of the three components of supersonic jet noise. In addition, we also developed a computational method for calculating the mean flow of turbulent high-speed jets. Below is a short description of the highlights of our contributions in each of these areas: (a) Broadband shock associated noise, (b) Turbulent mixing noise, (c) Screech tones and impingement tones, (d) Computation of the mean flow of turbulent jets.
- Document ID: 19980169273.
- No Copyright.
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