A nonlinear compressible flow disturbance formulation for adaptive mesh refinement wavepacket tracking in hypersonic boundary-layer flows
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Publication:2083878
DOI10.1016/j.compfluid.2022.105395OpenAlexW4221065165MaRDI QIDQ2083878
Hermann F. Fasel, Oliver M. F. Browne, Anthony P. Haas, Christoph Brehm
Publication date: 17 October 2022
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2022.105395
adaptive mesh refinementboundary-layer stabilityhypersonic boundary-layer transitionnonlinear disturbance formulationwave packet tracking
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Cites Work
- A locally stabilized immersed boundary method for the compressible Navier-Stokes equations
- A fast compact algorithm for cubic spline smoothing
- Analysis of the linear stability of compressible boundary layers using the PSE
- On a stabilization procedure for the parabolic stability equations
- A parallel three-dimensional computational aeroacoustics method using nonlinear disturbance equations
- On the nature of PSE approximation
- PARAMESH: A parallel adaptive mesh refinement community toolkit
- A comparison of higher-order finite-difference shock capturing schemes
- Reconstruction of turbulent fluctuations using a hybrid RANS/LES approach.
- An efficient linear wavepacket tracking method for hypersonic boundary-layer stability prediction
- A time-spectral approximate Jacobian based linearized compressible Navier-Stokes solver for high-speed boundary-layer receptivity and stability
- Receptivity of a supersonic boundary layer to solid particulates
- On the practical application of the PSE approach to linear stability analysis
- Numerical modelling of supersonic boundary-layer receptivity to solid particulates
- Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown
