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Scaling and modeling of three-dimensional, end-wall, turbulent boundary layers. ph.d. thesis - final report
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reshotko, E. Goldberg, U. C. |
| Copyright Year | 1984 |
| Description | The method of matched asymptotic expansion was employed to identify the various subregions in three dimensional, turbomachinery end wall turbulent boundary layers, and to determine the proper scaling of these regions. The two parts of the b.l. investigated are the 3D pressure driven part over the endwall, and the 3D part located at the blade/end wall juncture. Models are proposed for the 3d law of the wall and law of the wake. These models and the data of van den Berg and Elsenaar and of Mueller are compared and show good agreement between models and experiments. |
| File Size | 1907584 |
| Page Count | 140 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840017873 |
| Archival Resource Key | ark:/13960/t0bw29s90 |
| Language | English |
| Publisher Date | 1984-06-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Fluid Mechanics Scaling Laws Wall Flow Turbulent Boundary Layer Turbomachinery Dynamic Models Mathematical Models Three Dimensional Boundary Layer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Thesis |
