1975
DOI: 10.1071/ph750395
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Overdriven Supersonic Heat Waves

Abstract: If a supersonic heat wave is overtaken by a shock, either generated externally or'induced by the sudden cooling of the wave front, an overdriven heat wave is formed which is similar to an overdriven detonation. The Mach number of the overdrlven heat wave is proportional to the product of the Mach numbers of the pursuing shock and the heat wave.

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“…where the factor q defines the energy per unit mass delivered to the fluid particles in case of considering exothermic effects (q > 0) or the energy per unit mass subtracted to the fluid particles when endothermic effects are considered (q < 0). In general, there exists the possibility of having three different functions for the first adiabatic exponent Γ 1 = (∂lnp)/(∂lnρ) ad , the ratio of the specific heats γ = c p /c v , and the enthalpy coefficient g, as occurs in partially dissociated or ionized gases [67,68]. The definition of the latter g = h/e = h/ (h − p/ρ), where h and e are the specific enthalpy and internal energy, respectively.…”
Section: A Base Flow Equationsmentioning
confidence: 99%
“…where the factor q defines the energy per unit mass delivered to the fluid particles in case of considering exothermic effects (q > 0) or the energy per unit mass subtracted to the fluid particles when endothermic effects are considered (q < 0). In general, there exists the possibility of having three different functions for the first adiabatic exponent Γ 1 = (∂lnp)/(∂lnρ) ad , the ratio of the specific heats γ = c p /c v , and the enthalpy coefficient g, as occurs in partially dissociated or ionized gases [67,68]. The definition of the latter g = h/e = h/ (h − p/ρ), where h and e are the specific enthalpy and internal energy, respectively.…”
Section: A Base Flow Equationsmentioning
confidence: 99%
“…This creates a rearward-facing, i.e. in the opposite direction to the IF, rarefaction wave and a forward-facing shock (Strachan and Ahlborn 1975;Ahlborn and Strachan 1973). Under homogeneous conditions and for an infinite flow stream these waves and shocks will form periodically (Schnerr & Adam 1997).…”
Section: Supersonic Ionization Fronts and Cooling Frontsmentioning
confidence: 99%