Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /
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| Author / Creator: | McVetta, Ashlie B., author. |
|---|---|
| Uniform title: | Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade (Revised copy) |
| Edition: | Revised copy. |
| Imprint: | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014. |
| Description: | 1 online resource (23 pages) : color illustrations. |
| Language: | English |
| Series: | NASA/TM ; 2013-218070/REV1 NASA technical memorandum ; 2013-218070/REV1. |
| Subject: | Supersonic turbines. Turbine blades. Aerodynamic heat transfer. Computational fluid dynamics. Reynolds number. Pressure distribution. Inlet flow. Angles (geometry) Angles (Geometry) Computational fluid dynamics. Reynolds number. |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10294880 |
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| 086 | 0 | |a NAS 1.15:2013-218070/REV.1 | |
| 100 | 1 | |a McVetta, Ashlie B., |e author. | |
| 240 | 1 | 0 | |a Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade (Revised copy) |
| 245 | 1 | 0 | |a Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / |c Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch. |
| 250 | |a Revised copy. | ||
| 264 | 1 | |a Cleveland, Ohio : |b National Aeronautics and Space Administration, Glenn Research Center, |c June 2014. | |
| 300 | |a 1 online resource (23 pages) : |b color illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA/TM ; |v 2013-218070/REV1 | |
| 500 | |a Title from title screen (viewed Dec. 1, 2014). | ||
| 500 | |a "June 2014." | ||
| 500 | |a "This revised copy, numbered as NASA/TM-2013-218070/REV1, June 2014, supersedes the previous version, NASA/TM-2013-218070, August 2013, in its entirety." | ||
| 500 | |a "AIAA-2012-3879." | ||
| 504 | |a Includes bibliographical references (page 23). | ||
| 536 | |a Sponsored by National Aeronautics and Space Administration |h WBS 380046.02.03.02.01.01 | ||
| 536 | |d E-18746-1 | ||
| 650 | 7 | |a Supersonic turbines. |2 nasat | |
| 650 | 7 | |a Turbine blades. |2 nasat | |
| 650 | 7 | |a Aerodynamic heat transfer. |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics. |2 nasat | |
| 650 | 7 | |a Reynolds number. |2 nasat | |
| 650 | 7 | |a Pressure distribution. |2 nasat | |
| 650 | 7 | |a Inlet flow. |2 nasat | |
| 650 | 7 | |a Angles (geometry) |2 nasat | |
| 650 | 7 | |a Angles (Geometry) |2 fast |0 http://id.worldcat.org/fast/fst00808869 | |
| 650 | 7 | |a Computational fluid dynamics. |2 fast |0 http://id.worldcat.org/fast/fst01745072 | |
| 650 | 7 | |a Reynolds number. |2 fast |0 http://id.worldcat.org/fast/fst01096833 | |
| 700 | 1 | |a Giel, Paul W., |e author. | |
| 700 | 1 | |a Welch, Gerard E., |e author. | |
| 710 | 2 | |a NASA Glenn Research Center, |e issuing body. |0 http://id.loc.gov/authorities/names/no99028434 |1 http://viaf.org/viaf/152765975 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e sponsoring body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 710 | 2 | |a Fundamental Aeronautics Program (U.S.), |e sponsoring body. |0 http://id.loc.gov/authorities/names/no2012002012 |1 http://viaf.org/viaf/222481864 | |
| 830 | 0 | |a NASA technical memorandum ; |v 2013-218070/REV1. | |
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