Vorticity generation and acoustic resonance of simulated solid rocket motor chamber with high wave number wall injection
From MaRDI portal
Publication:435371
DOI10.1016/J.COMPFLUID.2008.12.001zbMath1242.76307OpenAlexW2095156728MaRDI QIDQ435371
Publication date: 11 July 2012
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2008.12.001
Finite difference methods applied to problems in fluid mechanics (76M20) Hydro- and aero-acoustics (76Q05)
Cites Work
- Boundary conditions for direct simulations of compressible viscous flows
- Acoustically generated unsteady vorticity field in a long narrow cylinder with sidewall injection
- Coexisting acoustic-rotational flow in a cylinder with axisymmetric sidewall mass addition
- A Numerical Method for Solving the Equations of Compressible Viscous Flow
- Dissipative Two-Four Methods for Time-Dependent Problems
- Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
- Acoustically generated vorticity in an internal flow
- Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.
This page was built for publication: Vorticity generation and acoustic resonance of simulated solid rocket motor chamber with high wave number wall injection
