The present eort discusses multi-dimensional eigenvalue problems as applied to the solution of hydro-dynamic and aeroacoustic instability problems on complex geometries. As a demonstrator, global linear instability analyses of steady laminar ows on an elliptic cone in compressible ows are monitored; one such ow, obtained using a standard aerodynamics solver, is presented in gure 1. Flows on this geometry are intrinsically three-dimensional; as a matter of fact the three-dimensionality of the geometry of the elliptic cone accounts for the departure of the laminar-turbulent transition process from the fairly well-understood scenarios on circular cones 1 and other axisymmetric bodies of revolution. Shedding light on the essentially three-dim...
Control of linear flow instabilities has been demonstrated to be an effective theoretical flow contr...
AbstractModal three-dimensional BiGlobal linear instability analysis is performed in steady, spanwis...
Fluid flows that are smooth at low speeds become unstable and then turbulent at higher speeds. Th...
The present effort discusses multi-dimensional eigenvalue problems as applied to the solution of hyd...
Linear instability of complex flowsmay be analyzed by numerical solutions of partial-derivative-base...
DLR Institute of Aerodynamics and Flow Technology, BunsenstraX e 10, D-37073 G.ottingen, Germany A s...
Global linear instability theory is concerned with the temporal or spatial development of small-ampl...
Global linear instability theory is concerned with the temporal or spatial development of small-ampl...
The development of a general Jacobian-free approach for the solution of large-scale global linear in...
Non-modal linear stability analysis results are presented for hypersonic flow over an elliptic cone ...
AbstractThe existence of modal and non-modal linear three-dimensional global instabilities of spanwi...
Linear stability theory is concerned with the evolution of small-amplitude disturbances superimposed...
The linear instability of the three-dimensional boundary-layer over the HIFiRE-5 flight test geometr...
A version of the global Galerkin method applied to a wide range of hydrodynamic stability problems i...
Linear instability of complex ows may be analyzed by numerical solutions of partial-derivative-base...
Control of linear flow instabilities has been demonstrated to be an effective theoretical flow contr...
AbstractModal three-dimensional BiGlobal linear instability analysis is performed in steady, spanwis...
Fluid flows that are smooth at low speeds become unstable and then turbulent at higher speeds. Th...
The present effort discusses multi-dimensional eigenvalue problems as applied to the solution of hyd...
Linear instability of complex flowsmay be analyzed by numerical solutions of partial-derivative-base...
DLR Institute of Aerodynamics and Flow Technology, BunsenstraX e 10, D-37073 G.ottingen, Germany A s...
Global linear instability theory is concerned with the temporal or spatial development of small-ampl...
Global linear instability theory is concerned with the temporal or spatial development of small-ampl...
The development of a general Jacobian-free approach for the solution of large-scale global linear in...
Non-modal linear stability analysis results are presented for hypersonic flow over an elliptic cone ...
AbstractThe existence of modal and non-modal linear three-dimensional global instabilities of spanwi...
Linear stability theory is concerned with the evolution of small-amplitude disturbances superimposed...
The linear instability of the three-dimensional boundary-layer over the HIFiRE-5 flight test geometr...
A version of the global Galerkin method applied to a wide range of hydrodynamic stability problems i...
Linear instability of complex ows may be analyzed by numerical solutions of partial-derivative-base...
Control of linear flow instabilities has been demonstrated to be an effective theoretical flow contr...
AbstractModal three-dimensional BiGlobal linear instability analysis is performed in steady, spanwis...
Fluid flows that are smooth at low speeds become unstable and then turbulent at higher speeds. Th...