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Second sound shock waves and critical velocities in liquid helium 2Large amplitude second-sound shock waves were generated and the experimental results compared to the theory of nonlinear second-sound. The structure and thickness of second-sound shock fronts are calculated and compared to experimental data. Theoretically it is shown that at T = 1.88 K, where the nonlinear wave steepening vanishes, the thickness of a very weak shock must diverge. In a region near this temperature, a finite-amplitude shock pulse evolves into an unusual double-shock configuration consisting of a front steepened, temperature raising shock followed by a temperature lowering shock. Double-shocks are experimentally verified. It is experimentally shown that very large second-sound shock waves initiate a breakdown in the superfluidity of helium 2, which is dramatically displayed as a limit to the maximum attainable shock strength. The value of the maximum shock-induced relative velocity represents a significant lower bound to the intrinsic critical velocity of helium 2.
Document ID
19800008577
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Turner, T. N.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1979
Subject Category
Acoustics
Report/Patent Number
NASA-CR-162687
Report Number: NASA-CR-162687
Accession Number
80N16837
Funding Number(s)
CONTRACT_GRANT: NSG-7508
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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