Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds /
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| Author / Creator: | Plentovich, Elizabeth B. |
|---|---|
| Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1991. |
| Description: | 51 pages : illustrations ; 28 cm. |
| Language: | English |
| Series: | NASA technical paper ; 3099 NASA technical paper ; 3099. |
| Subject: | |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6505355 |
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| 100 | 1 | |a Plentovich, Elizabeth B. |0 http://id.loc.gov/authorities/names/n83156969 |1 http://viaf.org/viaf/75230612 | |
| 245 | 1 | 0 | |a Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds / |c E.B. Plentovich, Julio Chu, and M.B. Tracy. |
| 264 | 1 | |a [Washington, D.C.] : |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; |a [Springfield, Va.] : |b [For sale by the National Technical Information Service], |c 1991. | |
| 300 | |a 51 pages : |b illustrations ; |c 28 cm. | ||
| 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 | ||
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| 490 | 1 | |a NASA technical paper ; |v 3099 | |
| 500 | |a "July 1991"--Cover. | ||
| 538 | |a Available via Internet from the NTRS web site. Address as of 3/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910017810%5F1991017810.pdf; current access is available via PURL. | ||
| 504 | |a Includes bibliographical references (pages 5-6). | ||
| 650 | 0 | |a Aerodynamic load. |0 http://id.loc.gov/authorities/subjects/sh85001292 | |
| 650 | 0 | |a Aerodynamics, Transonic. |0 http://id.loc.gov/authorities/subjects/sh85001299 | |
| 650 | 0 | |a Cavities (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85021549 | |
| 650 | 0 | |a Reynolds number. |0 http://id.loc.gov/authorities/subjects/sh85113557 | |
| 650 | 0 | |a Turbulent boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85138754 | |
| 650 | 0 | |a Yawing (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85149046 | |
| 650 | 7 | |a Cavities. |2 nasat | |
| 650 | 7 | |a Flow distribution. |2 nasat | |
| 650 | 7 | |a High Reynolds number. |2 nasat | |
| 650 | 7 | |a Mach number. |2 nasat | |
| 650 | 7 | |a Pressure distribution. |2 nasat | |
| 650 | 7 | |a Subsonic flow. |2 nasat | |
| 650 | 7 | |a Transonic flow. |2 nasat | |
| 650 | 7 | |a Yaw. |2 nasat | |
| 700 | 1 | |a Chu, Julio. |0 http://id.loc.gov/authorities/names/n81030362 |1 http://viaf.org/viaf/6250464 | |
| 700 | 1 | |a Tracy, M. B. |1 http://viaf.org/viaf/104568199 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Program. |0 http://id.loc.gov/authorities/names/no91017593 |1 http://viaf.org/viaf/144531053 | |
| 830 | 0 | |a NASA technical paper ; |v 3099. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS67795 |y Government Publishing Office |
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