Boundary-layer effects on the reflection of sound waves and weak shock waves at shallow incidence
dc.contributor.author | Messiter, Arthur F. | en_US |
dc.date.accessioned | 2006-09-08T21:21:26Z | |
dc.date.available | 2006-09-08T21:21:26Z | |
dc.date.issued | 1977-09 | en_US |
dc.identifier.citation | Messiter, Arthur F.; (1977). "Boundary-layer effects on the reflection of sound waves and weak shock waves at shallow incidence." Zeitschrift für angewandte Mathematik und Physik ZAMP 28(5): 879-887. <http://hdl.handle.net/2027.42/43361> | en_US |
dc.identifier.issn | 0044-2275 | en_US |
dc.identifier.issn | 1420-9039 | en_US |
dc.identifier.uri | https://hdl.handle.net/2027.42/43361 | |
dc.description.abstract | When either a plane acoustic wave or a weak shock wave is incident upon an infinite wall, the boundary-layer correction to the reflected wave becomes large if the angle between the wave front and the normal to the wall approaches zero. It is shown that transformation to moving coordinates leads to transonic flow problems whose solution permits removal of the singular behavior in each of these cases. Wenn eine ebene Schallwelle oder ein schwacher Stoss so auf eine Wand auftrifft, dass der Winkel zwischen der Wellenfront und der Wandnormalen gegen Null geht, so wird die Korrektur der reflektierten Welle wegen der Wandgrenzschicht gross. In der vorliegenden Arbeit wird gezeigt, dass eine Transformation auf bewegte Koordinaten auf ein transonisches Problem führt, dessen Lösung die Singularität in beiden Fällen vermeidet. | en_US |
dc.format.extent | 423450 bytes | |
dc.format.extent | 3115 bytes | |
dc.format.mimetype | application/pdf | |
dc.format.mimetype | text/plain | |
dc.language.iso | en_US | |
dc.publisher | Birkhäuser-Verlag; Springer Science+Business Media | en_US |
dc.subject.other | Engineering | en_US |
dc.subject.other | Mathematical Methods in Physics | en_US |
dc.subject.other | Theoretical and Applied Mechanics | en_US |
dc.title | Boundary-layer effects on the reflection of sound waves and weak shock waves at shallow incidence | en_US |
dc.type | Article | en_US |
dc.subject.hlbsecondlevel | Mathematics | en_US |
dc.subject.hlbtoplevel | Science | en_US |
dc.description.peerreviewed | Peer Reviewed | en_US |
dc.contributor.affiliationum | Department of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USA | en_US |
dc.contributor.affiliationumcampus | Ann Arbor | en_US |
dc.description.bitstreamurl | http://deepblue.lib.umich.edu/bitstream/2027.42/43361/1/33_2005_Article_BF01603823.pdf | en_US |
dc.identifier.doi | http://dx.doi.org/10.1007/BF01603823 | en_US |
dc.identifier.source | Zeitschrift für angewandte Mathematik und Physik ZAMP | en_US |
dc.owningcollname | Interdisciplinary and Peer-Reviewed |
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