Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. Part II: Wall shear stress
dc.contributor.author | Liou, Meng-Sing | en_US |
dc.contributor.author | Adamson, Thomas Charles Jr. | en_US |
dc.date.accessioned | 2006-09-08T21:23:35Z | |
dc.date.available | 2006-09-08T21:23:35Z | |
dc.date.issued | 1980-03 | en_US |
dc.identifier.citation | Liou, M. S.; Adamson, T. C.; (1980). "Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. Part II: Wall shear stress." Zeitschrift für angewandte Mathematik und Physik ZAMP 31(2): 227-246. <http://hdl.handle.net/2027.42/43393> | en_US |
dc.identifier.issn | 0044-2275 | en_US |
dc.identifier.issn | 1420-9039 | en_US |
dc.identifier.uri | https://hdl.handle.net/2027.42/43393 | |
dc.description.abstract | Asymptotic methods are used to calculate the shear stress at the wall for the interaction between a normal shock wave and a turbulent boundary layer on a flat plate. A mixing length model is used for the eddy viscosity. The shock wave is taken to be strong enough that the sonic line is deep in the boundary layer and the upstream influence is thus very small. It is shown that unlike the result found for laminar flow an asymptotic criterion for separation is not found; however, conditions for incipient separation are computed numerically using the derived solution for the shear stress at the wall. Results are compared with available experimental measurements. Die Schubspannung entlang einer ebenen Platte wird mit asymptotischen Methoden gerechnet für den Fall, dass ein senkrechter Stoss auf die turbulente Grenzschicht einwirkt. Für die Rechnung wird ein Mischweg-Modell benützt. Der Stoss ist von solcher Stärke, dass die Schallinie tief in der Grenzschicht liegt, und so die Wirkung stromaufwärts sehr klein ist. Im Gegensatz zu der laminaren Strömung kann man in diesem Fall eine asymptotische Bedingung für Grenzschicht-Ablösung nicht finden. Aber die Bedingungen für den Beginn der Ablösung kann man von der Lösung für die Schubspannung an der Wand numerisch erhalten. Die Ergebnisse der Theorie werden mit den vorhandenen experimentellen Messresultaten verglichen. | en_US |
dc.format.extent | 1158323 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 | Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. Part II: Wall shear stress | 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 | Dept of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USA; Flight Sciences Dept, McDonnell Douglas Research Laboratories, Box 516, 63166, St. Louis, Missouri, USA | en_US |
dc.contributor.affiliationum | Dept 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/2027.42/43393/1/33_2005_Article_BF01590749.pdf | en_US |
dc.identifier.doi | http://dx.doi.org/10.1007/BF01590749 | en_US |
dc.identifier.source | Zeitschrift für angewandte Mathematik und Physik ZAMP | en_US |
dc.owningcollname | Interdisciplinary and Peer-Reviewed |
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