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Shock wave oscillation driven by turbulent boundary layer fluctuations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Plotkin, K. J. |
| Copyright Year | 1972 |
| Description | Pressure fluctuations due to the interaction of a shock wave with a turbulent boundary layer were investigated. A simple model is proposed in which the shock wave is convected from its mean position by velocity fluctuations in the turbulent boundary layer. Displacement of the shock is assumed limited by a linear restoring mechanism. Predictions of peak root mean square pressure fluctuation and spectral density are in excellent agreement with available experimental data. |
| File Size | 495409 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730003554 |
| Archival Resource Key | ark:/13960/t3tt9cr7j |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Shock Waves Flow Distribution Turbulent Boundary Layer Mathematical Models Equations of Motion Pressure Velocity Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
