Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model
dc.contributor.author | Cebeci, Tuncer | en_US |
dc.contributor.author | Jang, Hong-Ming | en_US |
dc.date.accessioned | 2010-06-11T18:17:06Z | |
dc.date.available | 2010-06-11T18:17:06Z | |
dc.date.issued | 1990 | en_US |
dc.identifier.citation | Cebeci, Tuncer; Jang, Hong-Ming (1990). "Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model" JOURNAL OF AIRCRAFT, vol.27 no.8 (673-678). <http://hdl.handle.net/2027.42/76445> | en_US |
dc.identifier.issn | 0021-8669 | en_US |
dc.identifier.uri | https://hdl.handle.net/2027.42/76445 | |
dc.format.extent | 737110 bytes | |
dc.format.extent | 3112 bytes | |
dc.format.mimetype | application/pdf | |
dc.format.mimetype | text/plain | |
dc.publisher | American Institute of Aeronautics and Astronautics | en_US |
dc.title | Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model | en_US |
dc.type | Article | en_US |
dc.subject.hlbsecondlevel | Aerospace Engineering | en_US |
dc.subject.hlbtoplevel | Engineering | en_US |
dc.description.peerreviewed | Peer Reviewed | en_US |
dc.contributor.affiliationum | Michigan, University, Ann Arbor | en_US |
dc.contributor.affiliationother | Douglas Aircraft Co., Long Beach, CA | en_US |
dc.description.bitstreamurl | http://deepblue.lib.umich.edu/bitstream/2027.42/76445/1/AIAA-25340-880.pdf | |
dc.identifier.doi | 10.2514/3.25340 | en_US |
dc.identifier.source | JOURNAL OF AIRCRAFT | en_US |
dc.owningcollname | Interdisciplinary and Peer-Reviewed |
Files in this item
Remediation of Harmful Language
The University of Michigan Library aims to describe library materials in a way that respects the people and communities who create, use, and are represented in our collections. Report harmful or offensive language in catalog records, finding aids, or elsewhere in our collections anonymously through our metadata feedback form. More information at Remediation of Harmful Language.
Accessibility
If you are unable to use this file in its current format, please select the Contact Us link and we can modify it to make it more accessible to you.