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Experiments on an unsteady, three-dimensional separation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Henk, R. W. Reynolds, W. C. Reed, H. L. |
| Copyright Year | 1992 |
| Description | Unsteady, three-dimensional flow separation occurs in a variety of technical situations including turbomachinery and low-speed aircraft. An experimental program at Stanford in unsteady, three-dimensional, pressure-driven laminar separation has investigated the structure and time-scaling of these flows; of particular interest is the development, washout, and control of flow separation. Results reveal that a two-dimensional, laminar boundary layer passes through several stages on its way to a quasi-steady three-dimensional separation. The quasi-steady state of the separation embodies a complex, unsteady, vortical structure. |
| File Size | 679086 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940030475 |
| Archival Resource Key | ark:/13960/t7xm3791v |
| Language | English |
| Publisher Date | 1992-03-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Boundary Layer Separation Laminar Boundary Layer Two Dimensional Boundary Layer Three Dimensional Flow Low Speed Turbomachinery Quasi-steady States Unsteady Flow Separated Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
