Some rotational corrections to the acoustic energy equation in injection-driven enclosures

DOI10.1063/1.1920647zbMath1187.76328OpenAlexW2090783981MaRDI QIDQ3555164

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

Publication date: 22 April 2010

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

Full work available at URL: https://semanticscholar.org/paper/370f78fa5581d818de64bfda029ea46446ae587b

zbMATH Keywords

vorticesMach numberflow instabilitynozzlesflow through porous media

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (4)

Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift ⋮ Acoustic streaming in simplified liquid rocket engines with transverse mode oscillations ⋮ On steady rotational high speed flows: the compressible Taylor–Culick profile ⋮ Asymptotically based self-similarity solution of the Navier–Stokes equations for a porous tube with a non-circular cross-section

Cites Work

• The oscillatory channel flow with large wall injection
• Laminar cold-flow model for the internal gas dynamics of a slab rocket motor
• On the dependence on the formulation of some nonparallel stability approaches applied to the Taylor flow
• On the nonparallel stability of the injection induced two-dimensional Taylor flow
• Receptivity and aeroacoustic resonance in channels with blowing walls
• Flow turning in solid-propellant rocket combustion stability analyses
• Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
• The oscillatory pipe flow with arbitrary wall injection
• Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.

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