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Heat transfer in serpentine passages with turbulence promoters
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Boyle, R. J. |
| Copyright Year | 1984 |
| Description | Local heat transfer rates and overall pressure losses were determined for serpentine passages of square cross section. The flow entered an inlet leg, turned 180 deg and then passed through an outlet leg. Results were obtained for a passage with smooth walls for three different bend geometries and the effect of turbulence promoters was investigated. Turbulence promoters between 0.6 and 15% of the passage height were tested. Local heat transfer rates are determined from thermocouple measurements on a thin electrically heated Inconel foil and pressure drop is measured along the flow path. |
| File Size | 32540899 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840014843 |
| Archival Resource Key | ark:/13960/t3sv2f20d |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Thrust Augmentation Thermohydraulics Turbulent Flow Turbulent Heat Transfer Rotor Blades Turbomachinery Pressure Drop Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
