1969
DOI: 10.1017/s0022112069000590
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On the structure of a class of aerothermodynamic shocks

Abstract: Some recent work on the existence of vibrational de-excitation shocks (δ-shocks) in expanding non-equilibrium nozzle flows is extended to include situations in which an adiabatic shock (δ-shocks) may be embedded within the de-excitation shock. A discussion of some further properties of the shock solution is given and some examples are worked out. Numerical solutions of the full equations are also presented. These solutions confirm the existence of the δ-shocks but bring to light certain anomalies in the simple… Show more

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Cited by 1 publication
(4 citation statements)
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“…The precursor to this motion will still be described by the non-linear theory of $4.4.1 in general. All of these results are originally due to Blythe (1969) and illustrate something of the complexities introduced into otherwise elementary flow situations by the presence of relaxation. However, one is not finished yet as the results in this and in the previous subsection imply a limitation on the size of (a2-1).…”
Section: 42mentioning
confidence: 91%
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“…The precursor to this motion will still be described by the non-linear theory of $4.4.1 in general. All of these results are originally due to Blythe (1969) and illustrate something of the complexities introduced into otherwise elementary flow situations by the presence of relaxation. However, one is not finished yet as the results in this and in the previous subsection imply a limitation on the size of (a2-1).…”
Section: 42mentioning
confidence: 91%
“…The situation covered by these approximate deductions can be recognised as wholly consistent with the exact results of Q3.2 and 4.1, and it actually extends these results in numerous helpful ways; it also constitutes the analytical counterpart to the numerical computations outlined briefly in $4.2. There are some limitations, which it is not vital to make explicit here, especially since there are some more, strongly-related, matters to follow, but the interested reader can consult the original work by Blythe (1969) or any of the reviews and developments by Lick (1970), Becker (1972) and Clarke and McChesney (1976).…”
Section: Non-linear Efects In Small Disturbance Jieldsmentioning
confidence: 99%
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