Acoustic streaming in simplified liquid rocket engines with transverse mode oscillations

DOI10.1063/1.3407663zbMath1190.76040OpenAlexW2032635572MaRDI QIDQ3578618

Sean R. Fischbach, Gary A. Flandro, Joseph Majdalani

Publication date: 20 July 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/199c420b4395ab70636f25ab60a3b4fdc17d5207

zbMATH Keywords

boundary layersrotational flow

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

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• A hybrid multiple scale procedure for boundary layers involving several dissimilar scales
• The blowhard problem - inviscid flows with surface injection
• The oscillatory channel flow with large wall injection
• Some rotational corrections to the acoustic energy equation in injection-driven enclosures
• Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
• The oscillatory pipe flow with arbitrary wall injection
• Improved energy normalization function in rocket motor stability calculations
• Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift
• The oscillatory channel flow with arbitrary wall injection.

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