J. Peraire† Massachusetts Institute of Technology / American Institute of Aeronautics / /
IndustryTerm
oscillatory solution / hyperbolic nonlinear systems / hypersonic applications / transonic and supersonic applications / inner products / correct and stable solution / internal energy / approximate solution / gas dynamics / smooth solution / steady-state solution / numerical solution / energy / /
NaturalFeature
inlet Mach / Astronautics inlet / /
Organization
American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / Singapore-MIT Alliance / Air Force office of Scientific Research / Massachusetts Institute of Technology / American Institute of Aeronautics and Astronautics To / Department of Aeronautics and Astronautics / American Institute of Aeronautics and Astronautics Pm Pm Pd / /
Person
David Moro / Bernardo Cockburn / /
Position
hb / Research Scientist / Professor / artificial viscosity model for stronger shocks / representative / /
An Adaptive Shock-Capturing HDG Method for Compressible Flows