Improved Time-Dependent Flowfield Solution for Solid Rocket Motors

DOI10.2514/2.7507zbMath0900.70107OpenAlexW1996538386MaRDI QIDQ4393059

William K. van Moorhem, Joseph Majdalani

Publication date: 1 November 1998

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/2.7507

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (9)

Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift ⋮ Multiple asymptotic solutions for axially travelling waves in porous channels ⋮ Vorticity generation and acoustic resonance of simulated solid rocket motor chamber with high wave number wall injection ⋮ Coexisting acoustic-rotational flow in a cylinder with axisymmetric sidewall mass addition ⋮ Some rotational corrections to the acoustic energy equation in injection-driven enclosures ⋮ Three-dimensional flow in a cylinder with sidewall mass addition ⋮ Acoustic streaming in simplified liquid rocket engines with transverse mode oscillations ⋮ On steady rotational high speed flows: the compressible Taylor–Culick profile ⋮ Direct numerical simulation and biglobal stability investigations of the gaseous motion in solid rocket motors

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