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NACA-TN-2836
Radiant-interchange configuration factors
Year: 1952
Abstract: A study is presented of the geometric configuration factors required for computing radiant heat transfer between opaque surfaces separated by a nonabsorbing medium and various methods of determining the configuration factors are discussed. Configuration-factor solutions available in the literature have been checked and the more complicated equations are presented as families of curves. Cases for point, line, and finite-area sources are worked out over a wide range of geometric proportions. These cases include several new configurations involving rectangles, triangles, and cylinders of finite length which are integrated and tabulated. An analysis is presented, in which configuration factors are employed of the radiant heat transfer to the rotor blades of a typical gas turbine under different conditions of temperature and pressure. (author)
Subject: ABSORPTION
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:09:43Z | |
| date available | 2017-09-04T18:09:43Z | |
| date copyright | 01/01/1952 | |
| date issued | 1952 | |
| identifier other | GVONEEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho16/handle/yse/192812 | |
| description abstract | A study is presented of the geometric configuration factors required for computing radiant heat transfer between opaque surfaces separated by a nonabsorbing medium and various methods of determining the configuration factors are discussed. Configuration-factor solutions available in the literature have been checked and the more complicated equations are presented as families of curves. Cases for point, line, and finite-area sources are worked out over a wide range of geometric proportions. These cases include several new configurations involving rectangles, triangles, and cylinders of finite length which are integrated and tabulated. An analysis is presented, in which configuration factors are employed of the radiant heat transfer to the rotor blades of a typical gas turbine under different conditions of temperature and pressure. (author) | |
| language | English | |
| title | NACA-TN-2836 | num |
| title | Radiant-interchange configuration factors | en |
| type | standard | |
| page | 111 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1952 | |
| contenttype | fulltext | |
| subject keywords | ABSORPTION | |
| subject keywords | AIRCRAFT ENGINES | |
| subject keywords | ANALYSIS (MATHEMATICS) | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | COOLING | |
| subject keywords | CYLINDERS | |
| subject keywords | EMISSIVITY | |
| subject keywords | GAS TURBINE ENGINES | |
| subject keywords | GASES | |
| subject keywords | RADIATIVE HEAT TRANSFER | |
| subject keywords | RECTANGLES | |
| subject keywords | ROTOR BLADES (TURBOMACHINERY) | |
| subject keywords | SURFACE GEOMETRY | |
| subject keywords | TRIANGLES |