Experiments on turbulent boundary layers along a circular cylinder with and without separation
August 1967
| Main Authors: | , |
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| Format: | Technical Report |
| Published: |
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1967]
2016
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| Online Access: | http://hdl.handle.net/1721.1/104704 |
| _version_ | 1811070258040012800 |
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| author | Fernholz, Hans Gibson, Paul. Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author2 | Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine Laboratory Fernholz, Hans Gibson, Paul. Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_sort | Fernholz, Hans |
| collection | MIT |
| description | August 1967 |
| first_indexed | 2024-09-23T08:33:37Z |
| format | Technical Report |
| id | mit-1721.1/104704 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T08:33:37Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1967] |
| record_format | dspace |
| spelling | mit-1721.1/1047042019-04-08T07:21:34Z Experiments on turbulent boundary layers along a circular cylinder with and without separation Fernholz, Hans Gibson, Paul. Massachusetts Institute of Technology. Gas Turbine Laboratory Massachusetts Institute of Technology. Gas Turbine Laboratory TA357 .F47x Turbulent boundary layer Fluid mechanics Cylinders August 1967 Includes bibliographical references Summary: Experiments were conducted in a turbulent boundary-layer near separation along a circular cylinder with the flow in the axial direction. The pressure gradient along the axis of the cylinder could be varied such that it was possible to maintain three boundary-layer configurations close to separation or with regions of reversed flow: 1. A turbulent boundary-layer with skin friction zero. 2. A turbulent boundary layer with a separated region and reattachment further downstream with skin friction zero. 3. A turbulent boundary layer with a region of small but constant skin friction and normal separation. Pressure and skin friction along the cylinder wall,. as well as mean velocity profiles in the boundary-layer, were measured. Research carried out under Bureau Of Ships General Hydromechanics Research Program, S-R009 01 01 Administered by the David Taylor Model Basin Contract Nonr 1841 (91) 2016-10-06T21:22:03Z 2016-10-06T21:22:03Z 1967 Technical Report http://hdl.handle.net/1721.1/104704 08456869 14173837 GTL report #91 [73] pages in various foliations Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1967] |
| spellingShingle | TA357 .F47x Turbulent boundary layer Fluid mechanics Cylinders Fernholz, Hans Gibson, Paul. Massachusetts Institute of Technology. Gas Turbine Laboratory Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title | Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title_full | Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title_fullStr | Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title_full_unstemmed | Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title_short | Experiments on turbulent boundary layers along a circular cylinder with and without separation |
| title_sort | experiments on turbulent boundary layers along a circular cylinder with and without separation |
| topic | TA357 .F47x Turbulent boundary layer Fluid mechanics Cylinders |
| url | http://hdl.handle.net/1721.1/104704 |
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