A modeling technique for STOVL ejector and volume dynamics /
Saved in:
| Author / Creator: | Drummond, Colin K. |
|---|---|
| Imprint: | [Washington, D.C.] : NASA ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [1990] |
| Description: | 11 pages : illustrations. |
| Language: | English |
| Series: | NASA technical memorandum ; 103167 NASA technical memorandum ; 103167. |
| Subject: | |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6504502 |
MARC
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| 086 | 0 | |a NAS 1.15:103167 | |
| 088 | |a AIAA-90-2417 | ||
| 088 | |a E-5539 | ||
| 100 | 1 | |a Drummond, Colin K. |0 http://id.loc.gov/authorities/names/no2007091060 |1 http://viaf.org/viaf/7175000 | |
| 245 | 1 | 2 | |a A modeling technique for STOVL ejector and volume dynamics / |c C.K. Drummond and W.S. Barankiewicz ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990. |
| 264 | 1 | |a [Washington, D.C.] : |b NASA ; |a [Springfield, Va. :] : |b [For sale by the National Technical Information Service], |c [1990] | |
| 300 | |a 11 pages : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
| 338 | |a microfiche |b he |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/he | ||
| 490 | 1 | |a NASA technical memorandum ; |v 103167 | |
| 500 | |a Cover title. | ||
| 538 | |a Available via Internet from the NASA Technical Report Server web site. Address as of 1/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013250%5F1990013250.pdf; current access available via PURL. | ||
| 504 | |a Includes bibliographical references (pages 7-8). | ||
| 500 | |a "AIAA-90-2417." | ||
| 500 | |a "E-5539"--P. 1. | ||
| 536 | |h 505-62-71 | ||
| 650 | 0 | |a Short take-off and landing aircraft |x Jet propulsion |x Ejectors |x Mathematical models. | |
| 650 | 7 | |a Aircraft configurations. |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics. |2 nasat | |
| 650 | 7 | |a Mathematical models. |2 nasat | |
| 650 | 7 | |a Performance prediction. |2 nasat | |
| 650 | 7 | |a Thrust. |2 nasat | |
| 650 | 7 | |a V/STOL aircraft. |2 nasat | |
| 700 | 1 | |a Barankiewicz, W. S. | |
| 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 103167. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS66379 |y Government Publishing Office |
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| 929 | |a eresource | ||
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/LPS66379 |z Government Publishing Office |g ebooks |i 12738669 | ||