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User's guide and description of the streamline divergence computer program. [turbulent convective heat transfer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McAnally, J. V. Sulyma, P. R. |
| Copyright Year | 1975 |
| Description | The streamline divergence program was developed to demonstrate the capability to trace inviscid surface streamlines and to calculate outflow-corrected laminar and turbulent convective heating rates on surfaces subjected to exhaust plume impingement. The analytical techniques used in formulating this program are discussed. A brief description of the streamline divergence program is given along with a user's guide. The program input and output for a sample case are also presented. |
| File Size | 1001992 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750011519 |
| Archival Resource Key | ark:/13960/t52g2h646 |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Convective Heat Transfer Turbulent Heat Transfer Laminar Flow Impingement Flow Distribution Inviscid Flow Flow Characteristics Rocket Exhaust Computer Programs 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 |
