Aeromechanics analysis of a boundary layer ingesting fan /
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| Author / Creator: | Bakhle, Milind A., author. |
|---|---|
| Imprint: | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013. |
| Description: | 1 online resource (15 pages) : color illustrations. |
| Language: | English |
| Series: | NASA/TM ; 2013-217730 NASA technical memorandum ; 217730. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10292971 |
MARC
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| 100 | 1 | |a Bakhle, Milind A., |e author. |0 http://id.loc.gov/authorities/names/no2003043373 |1 http://viaf.org/viaf/76002937 | |
| 245 | 1 | 0 | |a Aeromechanics analysis of a boundary layer ingesting fan / |c Milind A. Bakhle [and four others]. |
| 264 | 1 | |a Cleveland, Ohio : |b National Aeronautics and Space Administration, Glenn Research Center, |c 2013. | |
| 300 | |a 1 online resource (15 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 2013-217730 | |
| 500 | |a Title from title screen (viewed on Aug. 25, 2014). | ||
| 500 | |a "January 2013." | ||
| 500 | |a "Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Atlanta, Georgia, July 30-August 1, 2012." | ||
| 504 | |a Includes bibliographical references (page 15). | ||
| 536 | |a Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center |h WBS 561581.02.08.03.47.03.01 | ||
| 536 | |d AIAA Paper 2012-3995 |d E-18442 | ||
| 650 | 7 | |a Computational fluid dynamics. |2 nasat | |
| 650 | 7 | |a Dynamic loads. |2 nasat | |
| 650 | 7 | |a Propulsion system configurations. |2 nasat | |
| 650 | 7 | |a Inlet flow. |2 nasat | |
| 650 | 7 | |a Propulsion system performance. |2 nasat | |
| 650 | 7 | |a Reynolds averaging. |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics. |2 fast |0 http://id.worldcat.org/fast/fst01745072 | |
| 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 | 2 | |a Fundamental Aeronautics Program (U.S.), |e sponsoring body. |0 http://id.loc.gov/authorities/names/no2012002012 |1 http://viaf.org/viaf/222481864 | |
| 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 | |
| 830 | 0 | |a NASA technical memorandum ; |v 217730. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo51528 |y GPO Documents Without Shelves |
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