TY - GEN
T1 - Matrix extraction technique for global stability of compressible flows and applications
AU - De Pando, Miguel Fosas
AU - Sipp, Denis
AU - Schmid, Peter J.
N1 - Generated from Scopus record by KAUST IRTS on 2022-09-13
PY - 2011/12/1
Y1 - 2011/12/1
N2 - The derivation of the linearized operator for large-scale flow problems is a cumbersome and error-prone task, especially regarding the adjoint. The complexity of compressible direct numerical simulations and the use of high-order discretizations complicate the application of efficient procedures. Nevertheless, both operators are at the core of numerous algorithms for quantitative flow analysis; thus providing access to them is of great practical interest. A novel algorithm based on a divide and conquer strategy for the extraction and evaluation of the linearized operators, from a nonlinear flow solver, is presented. This technique is demonstrated on an existing compressible flow solver and validated by the computation of global modes in a spatially developing boundary layer. Finally, potential applications will be illustrated by the computation of the most unstable direct and adjoint global modes in the flow around an airfoil. Copyright © 2011 by the author(s).
AB - The derivation of the linearized operator for large-scale flow problems is a cumbersome and error-prone task, especially regarding the adjoint. The complexity of compressible direct numerical simulations and the use of high-order discretizations complicate the application of efficient procedures. Nevertheless, both operators are at the core of numerous algorithms for quantitative flow analysis; thus providing access to them is of great practical interest. A novel algorithm based on a divide and conquer strategy for the extraction and evaluation of the linearized operators, from a nonlinear flow solver, is presented. This technique is demonstrated on an existing compressible flow solver and validated by the computation of global modes in a spatially developing boundary layer. Finally, potential applications will be illustrated by the computation of the most unstable direct and adjoint global modes in the flow around an airfoil. Copyright © 2011 by the author(s).
UR - http://www.scopus.com/inward/record.url?scp=84871864270&partnerID=8YFLogxK
M3 - Conference contribution
SN - 9781624101441
BT - 6th AIAA Theoretical Fluid Mechanics Conference
ER -