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Fortran program for calculating coolant flow and metal temperatures of a full-coverage-film-cooled vane or blade
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Meitner, P. L. |
| Copyright Year | 1978 |
| Description | A computer program that calculates the coolant flow and the metal temperatures of a full-coverage-film-cooled vane or blade was developed. The analysis was based on compressible, one-dimensional fluid flow and on one-dimensional heat transfer and treats the vane or blade shell as a porous wall. The calculated temperatures are average values for the shell outer-surface area associated with each film-cooling hole row. A thermal-barrier coating may be specified on the shell outer surface, and centrifugal effects can be included for blade calculations. The program is written in FORTRAN 4 and is operational on a UNIVAC 1100/42 computer. The method of analysis, the program input, the program output, and two sample problems are provided. |
| File Size | 3102186 |
| Page Count | 93 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780020156 |
| Archival Resource Key | ark:/13960/t1rg0j99q |
| Language | English |
| Publisher Date | 1978-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Turbine Blades Metal Surfaces Fluid Flow Vanes Coolants Film Cooling Heat Transfer Univac 1100 Series Computers Computer Programs Fortran Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |