Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift

DOI10.1063/1.2746042zbMath1182.76249OpenAlexW2132652589MaRDI QIDQ5303447

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

Publication date: 18 March 2010

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

Full work available at URL: https://semanticscholar.org/paper/18644357c04666d576b7608f0c015005fdffbd05

zbMATH Keywords

stabilitycombustionrocket engines

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (5)

On the swirling Trkalian mean flow field in solid rocket motors ⋮ Acoustic streaming in simplified liquid rocket engines with transverse mode oscillations ⋮ Thermoacoustic instability in a solid rocket motor: non-normality and nonlinear instabilities ⋮ Asymptotically based self-similarity solution of the Navier–Stokes equations for a porous tube with a non-circular cross-section ⋮ Weakly nonlinear analysis of thermoacoustic bifurcations in the Rijke tube

Cites Work

• The oscillatory channel flow with large wall injection
• Some rotational corrections to the acoustic energy equation in injection-driven enclosures
• Flow turning in solid-propellant rocket combustion stability analyses
• Some recent results for nonlinear acoustics in combustion chambers
• Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
• Resonant oscillations in closed tubes

This page was built for publication: Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift