Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /
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| Author / Creator: | Jones, Kenneth M., author. |
|---|---|
| Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, [1995] |
| Description: | 1 online resource (25 pages) : illustrations. |
| Language: | English |
| Series: | NASA-TM ; 112005 NASA technical memorandum ; 112005. |
| Subject: | Aerodynamic configurations. Airfoils. Computational fluid dynamics. Navier-Stokes equation. Reynolds number. Wing flaps. Aerofoils. 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/11288384 |
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| 035 | |a (OCoLC)990788328 | ||
| 040 | |a GPO |b eng |e rda |e pn |c GPO |d GPO |d MvI | ||
| 074 | |a 0830-D (online) | ||
| 086 | 0 | |a NAS 1.15:112005 | |
| 088 | |a AIAA 95-1855 | ||
| 100 | 1 | |a Jones, Kenneth M., |e author. |0 http://id.loc.gov/authorities/names/n50041062 |1 http://viaf.org/viaf/241535832 | |
| 245 | 1 | 0 | |a Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques / |c Kenneth M. Jones, Robert T. Biedron, Mark Whitlock. |
| 264 | 1 | |a [Washington, D.C.] : |b National Aeronautics and Space Administration, |c [1995] | |
| 300 | |a 1 online resource (25 pages) : |b 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 112005 | |
| 500 | |a "13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California." | ||
| 500 | |a "AIAA 95-1855." | ||
| 504 | |a Includes bibliographical references (page 12). | ||
| 588 | |a Description based on online resource; title from PDF title page (NASA, viewed June 22, 2017). | ||
| 650 | 7 | |a Aerodynamic configurations. |2 nasat | |
| 650 | 7 | |a Airfoils. |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics. |2 nasat | |
| 650 | 7 | |a Navier-Stokes equation. |2 nasat | |
| 650 | 7 | |a Reynolds number. |2 nasat | |
| 650 | 7 | |a Wing flaps. |2 nasat | |
| 650 | 7 | |a Aerofoils. |2 fast |0 http://id.worldcat.org/fast/fst00798241 | |
| 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 Biedron, Robert T., |e author. |0 http://id.loc.gov/authorities/names/no00104262 |1 http://viaf.org/viaf/19234363 | |
| 700 | 1 | |a Whitlock, Mark, |e author. | |
| 710 | 2 | |a American Institute of Aeronautics and Astronautics. |0 http://id.loc.gov/authorities/names/n79053067 |1 http://viaf.org/viaf/155786255 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e issuing body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 776 | 0 | 8 | |i Print version: |t Application of a navier-stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques |w (OCoLC)62404812 |
| 776 | 0 | 8 | |i Microfiche version: |a Jones, Kenneth M. |t Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques |w (OCoLC)46763288 |
| 830 | 0 | |a NASA technical memorandum ; |v 112005. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo77771 |y GPO Documents Without Shelves |
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u http://purl.fdlp.gov/GPO/gpo77771 |z GPO Documents Without Shelves |g ebooks |i 10146986 | ||