Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile /
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Author / Creator: | Stabe, Roy G. |
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Imprint: | [Washington, D.C.] : [National Aeronautics and Space Administration], [1984] |
Description: | 1 volume. |
Language: | English |
Series: | NASA technical memorandum ; 83655 NASA technical memorandum ; 83655. |
Subject: | |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7259434 |
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100 | 1 | |a Stabe, Roy G. |0 http://id.loc.gov/authorities/names/n83163177 |1 http://viaf.org/viaf/48143771 | |
245 | 1 | 0 | |a Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile / |c Roy G. Stabe, Warren J. Whitney, and Thomas P. Moffitt. |
246 | 3 | |a Performance of a high work, low aspect ratio ... | |
264 | 1 | |a [Washington, D.C.] : |b [National Aeronautics and Space Administration], |c [1984] | |
300 | |a 1 volume. | ||
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337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
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490 | 1 | |a NASA technical memorandum ; |v 83655 | |
538 | |a Available via Internet from the NTRS web site. Address as of 08/07/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840016521%5F1984016521.pdf ; current access is available via PURL. | ||
650 | 0 | |a Turbines |x Testing. | |
650 | 0 | |a Axial flow. | |
650 | 7 | |a Axial flow. |2 nasat | |
650 | 7 | |a Low aspect ratio. |2 nasat | |
650 | 7 | |a Temperature profiles. |2 nasat | |
650 | 7 | |a Turbine blades. |2 nasat | |
650 | 7 | |a Turbine engines. |2 nasat | |
700 | 1 | |a Whitney, Warren J. |0 http://id.loc.gov/authorities/names/n81021696 |1 http://viaf.org/viaf/30854494 | |
700 | 1 | |a Moffitt, Thomas P. |0 http://id.loc.gov/authorities/names/n81046645 |1 http://viaf.org/viaf/28392541 | |
710 | 1 | |a United States. |b National Aeronautics and Space Administration. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
776 | 0 | 8 | |i Paper version: |a Stabe, Roy G. |t Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile. |h 1 v.(various pagings). |w (OCoLC)699742736 |
830 | 0 | |a NASA technical memorandum ; |v 83655. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS99490 |y Government Publishing Office |
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