View Item 

Show simple item record

On the Interaction of Two Plane Shocks Facing in the Same Direction
dc.contributor.authorLaporte, Ottoen_US
dc.contributor.authorTurner, Eugene Bonneren_US
dc.date.accessioned2010-05-06T21:01:49Z
dc.date.available2010-05-06T21:01:49Z
dc.date.issued1954-05en_US
dc.identifier.citationLaporte, Otto; Turner, E. B. (1954). "On the Interaction of Two Plane Shocks Facing in the Same Direction." Journal of Applied Physics 25(5): 678-678. <http://hdl.handle.net/2027.42/69716>en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/69716
dc.format.extent3102 bytes
dc.format.extent407173 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.publisherThe American Institute of Physicsen_US
dc.rights© The American Institute of Physicsen_US
dc.titleOn the Interaction of Two Plane Shocks Facing in the Same Directionen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumRandall Laboratory of Physics, University of Michigan, Ann Arbor, Michiganen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/69716/2/JAPIAU-25-5-678-1.pdf
dc.identifier.doi10.1063/1.1721713en_US
dc.identifier.sourceJournal of Applied Physicsen_US
dc.identifier.citedreferenceJ. von Neumann, Progress Report on the Theory of Shock Waves. National Defense Research Committee, Division 8, Office of Scientific Research and Development No. 1140, 1943.en_US
dc.identifier.citedreferenceR. Courant and K. O. Friedrichs, Interaction of Shock and Rarefaction Waves in One‐Dimensional Motion. National Defense Research Committee, Applied Mathematics Panel Report 38.1R (Applied Mathematics Group—New York University No. 1), 1943.en_US
dc.identifier.citedreferenceBull, Fowell, and Henshaw, The Interaction of Two Similarly Facing Shock Waves. Institute of Aerophysics, University of Toronto, UTIA Report No. 25, 1953.en_US
dc.identifier.citedreferenceSince the plate stack did not span the height of the tube entirely, but left slightly more than 1 inch at top and bottom, the shocks show a slight curvature, especially at their ends and at the larger distances from the reflecting plates.en_US
dc.owningcollnamePhysics, Department of


Files in this item

Name:
JAPIAU-25-5-678-1.pdf
Size:
397.6KB
Format:
PDF
View/Open

Show simple item record

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.