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Gas side heat transfer: 2-d flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | York, R. |
| Copyright Year | 1982 |
| Description | Significant progress was made in advancing the idea of establishing a unified approach for predicting airfoil heat transfer for a wide range of operating conditions and geometries. Preliminary results are encouraging and further mixing length (ml) turbulence modeling ideas will be explored, concentrating on transition behavior. The capability of available modeling techniques to predict airfoil surface heat transfer distributions in a two-dimensional flow field was assessed, experimental data as required for model verification were acquired, and improvements in the analytic models was made and verified. |
| File Size | 431589 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850002657 |
| Archival Resource Key | ark:/13960/t9z07zd0k |
| Language | English |
| Publisher Date | 1982-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Finite Element Method Boundary Value Problems Gas Turbines Flow Distribution Stagnation Point Pressure Distribution Inviscid Flow Airfoils Two Dimensional Flow Prediction Analysis Techniques Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
