1977
DOI: 10.1016/0094-5765(77)90061-3
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Blast waves in real gases

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Cited by 7 publications
(5 citation statements)
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“…For the parameters tested here, the value Γ in the upper branch of the Hugoniot curve is always larger than the critical values for the onset of (a) shock instabilities associated with multi-wave 66,67 and multi-valued 68,69 solutions, and (b) D'yakov-Kontorovich pseudo-instabilities associated with the spontaneous emission of sound 8,70 . Similar characteristics of the Hugoniot curve have been observed elsewhere for shocks subjected to endothermicity [71][72][73][74] .…”
Section: The Turning Point In the Hugoniot Curve At Hypersonic Mach N...supporting
confidence: 82%
“…For the parameters tested here, the value Γ in the upper branch of the Hugoniot curve is always larger than the critical values for the onset of (a) shock instabilities associated with multi-wave 66,67 and multi-valued 68,69 solutions, and (b) D'yakov-Kontorovich pseudo-instabilities associated with the spontaneous emission of sound 8,70 . Similar characteristics of the Hugoniot curve have been observed elsewhere for shocks subjected to endothermicity [71][72][73][74] .…”
Section: The Turning Point In the Hugoniot Curve At Hypersonic Mach N...supporting
confidence: 82%
“…For the parameters tested here, the value Γ in the upper branch of the Hugoniot curve is always larger than the critical values for the onset of (a) shock instabilities associated with multi-wave [282,283] and multi-valued [284,285] solutions, and (b) D'yakov-Kontorovich pseudo-instabilities associated with the spontaneous emission of sound [49,[286][287][288][289]. Similar characteristics of the Hugoniot curve have been observed elsewhere for shocks subjected to endothermicity [289][290][291][292][293].…”
Section: Chapter 4 Thermochemical Effects On Hypersonic Shock Waves W...supporting
confidence: 74%
“…#1 In the prevailing number of cases, despite the extremely high temperatures prevailing close to the center of blast waves. the gas was treated in the literature as a calorically and thermally perfect one characterized by an appropriately selected adiabatic exponent y and gas constant R. On the other hand, from the results of the very few exceptions, e.g., Kamel et al (1976) or Komer (1991), it appears that temperature profiles are affected most by the real gas properties of the medium, while pressure and particle velocity and the decay of the shock front are relatively unaffected.…”
Section: Formulationmentioning
confidence: 99%