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Prediction of boundary-layer characteristics of an oscillating airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cebeci, T. Carr, L. W. |
| Copyright Year | 1981 |
| Description | The evolution of unsteady boundary layers on oscillating airfoils is investigated by solving the governing equations by the Characteristic Box scheme. The difficulties associated with computing the first profile on a given time line, and the velocity profiles with partial flow reversal are solved. A sample calculation is performed for an external velocity distribution typical of those found near the leading edge of thin airfoils. The viability of the calculation procedure is demonstrated. |
| File Size | 676248 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810019853 |
| Archival Resource Key | ark:/13960/t5s806772 |
| Language | English |
| Publisher Date | 1981-07-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Oscillating Flow Laminar Boundary Layer Airfoils Unsteady Flow Velocity Distribution Leading Edges Boundary Layers Boundary Layer Flow Pressure Gradients 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 |
