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A hot-wire surface gage for skin friction and separation detection measurements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Okuno, A. F. Rubesin, M. W. Brosh, A. Mateer, G. G. |
| Copyright Year | 1975 |
| Description | A heated-element, skin-friction gage employing a very low thermal conductivity support is described. It is shown that the effective dimension of the gage in the stream direction in only 0.06 mm, including the effects of heat conduction in the supporting material. Because of its small size, the calibration of the gage is independent of the kind of boundary-layer flow (whether laminar or turbulent) and is insensitive to pressure gradients. Construction tolerances can be maintained so that a single universal calibration can be applied. Multiple gages, sufficiently closely spaced so as to interfere with each other, are shown to provide accurate determinations of the locations of the points of boundary-layer separation and reattachment. |
| File Size | 1363979 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750021311 |
| Archival Resource Key | ark:/13960/t75t8dk9h |
| Language | English |
| Publisher Date | 1975-07-01 |
| Access Restriction | Open |
| Subject Keyword | Boundary Layer Separation Fluid Mechanics Conductive Heat Transfer Turbulent Flow Skin Friction Laminar Flow Calibrating Hot-wire Flowmeters Thermal Conductivity 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 |