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Analysis of a turbulent boundary layer over a moving ground plane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roper, A. T. Gentry Jr., G. L. |
| Copyright Year | 1972 |
| Description | Four methods of predicting the integral and friction parameters for a turbulent boundary layer over a moving ground plane were evaluated by using test information obtained in 76.2- by 50.8-centimeter tunnel. The tunnel was operated in the open sidewall configuration. These methods are (1) relative integral parameter method, (2) modified power law method, (3) relative power law method, and (4) modified law of the wall method. The modified law of the wall method predicts a more rapid decrease in skin friction with an increase in the ratio of belt velocity to free steam velocity than do methods (1) and (3). |
| File Size | 4966942 |
| Page Count | 75 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720018593 |
| Archival Resource Key | ark:/13960/t20c9qh1f |
| Language | English |
| Publisher Date | 1972-07-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Turbulent Boundary Layer Skin Friction Parameterization Free Flow Predictions 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 |
