2009
DOI: 10.1017/s0022112009007939
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Multiple asymptotic solutions for axially travelling waves in porous channels

Abstract: Travelling waves in confined enclosures, such as porous channels, develop boundary layers that evolve over varying spatial scales. The present analysis employs a technique that circumvents guessing of the inner coordinate transformations at the forefront of a multiple-scales expansion. The work extends a former study in which a two-dimensional oscillatory solution was derived for the rotational travelling wave in a porous channel. This asymptotic solution was based on a free coordinate that could be evaluated … Show more

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Cited by 38 publications
(51 citation statements)
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“…As shown by Majdalani, Vyas & Flandro (2002, 2009, the effects of time-dependent propellant grain regression on the mean flow may be safely dismissed in the context of linear stability and vorticoacoustic wave analysis. The characteristic frequencies of these unsteady effects are sufficiently low compared with other flow disturbances to justify ignoring them.…”
Section: Mean Flow Evaluationmentioning
confidence: 99%
See 1 more Smart Citation
“…As shown by Majdalani, Vyas & Flandro (2002, 2009, the effects of time-dependent propellant grain regression on the mean flow may be safely dismissed in the context of linear stability and vorticoacoustic wave analysis. The characteristic frequencies of these unsteady effects are sufficiently low compared with other flow disturbances to justify ignoring them.…”
Section: Mean Flow Evaluationmentioning
confidence: 99%
“…In this study, only a brief overview of the relevant theories will be presented. Substantially more detailed descriptions can be found in work by Chedevergne et al (2006) and Majdalani (2009).…”
Section: Theoretical Treatment Of Flow Disturbancesmentioning
confidence: 99%
“…This may be owed to its association with several studies involving hydrodynamic instability [23][24][25][26][27][28], acoustic instability [29][30][31][32][33][34][35], wave propagation [36][37][38][39], particle-mean flow interactions [40], and rocket performance measurements [41][42][43]. The Taylor-Culick solution was originally verified to be an adequate representation of the expected flowfield in SRMs both numerically by Sabnis et al [44] and experimentally by Dunlap et al [45,46], thereby confirming its character in a nonreactive chamber environment.…”
Section: Doi: 102514/1j055949mentioning
confidence: 95%
“…The instantaneous flow field plays a key role in describing acoustic instability, particle-mean flow interactions, erosive burning, nozzle erosion, and thrust performance. The traditional modus operandi is to decompose the instantaneous motion into a steady average flow and an amalgam of unsteady wave contributions (Chedevergne et al, 2007;Culick, 2006;Majdalani, 2009). In this context, the mean flow represents the bulk motion of the gases and can be approximated by the steady-state solution for a porous tube or channel with wall-normal injection.…”
Section: Relevance To Propulsion Systemsmentioning
confidence: 99%