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Effects of rotation on coolant passage heat transfer. volume 1: coolant passages with smooth walls
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Steuber, G. D. Wagner, J. H. Hajek, T. J. Higgins, A. W. Johnson, B. V. |
| Copyright Year | 1991 |
| Description | An experimental program was conducted to investigate heat transfer and pressure loss characteristics of rotating multipass passages, for configurations and dimensions typical of modern turbine blades. The immediate objective was the generation of a data base of heat transfer and pressure loss data required to develop heat transfer correlations and to assess computational fluid dynamic techniques for rotating coolant passages. Experiments were conducted in a smooth wall large scale heat transfer model. |
| File Size | 62689480 |
| Page Count | 140 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910021175 |
| Archival Resource Key | ark:/13960/t6rz45v2p |
| Language | English |
| Publisher Date | 1991-09-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Correlation Turbine Blades Computational Fluid Dynamics Scale Models Pressure Reduction Coolants Rotation Walls Heat Transfer Data Bases 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 |
