Orlando / Report / Cambridge / San Antonio / Honolulu / Hononulu / New York / /
Company
SIAM Journal / RANS Solutions / Fluid Dynamics Panel Working Group / Reno NV / McGraw-Hill / Aeronautics and Astronautics Inc. / /
Event
Force Majeure / Reorganization / /
Facility
N. C. Nguyen† Massachusetts Institute of Technology / Stanford University / University of Minnesota / American Institute of Aeronautics / USA B. Cockburn‡ University of Minnesota / /
IndustryTerm
numerical discretization algorithm / inner-law data / inner products / approximate solution / matrix systems / gas dynamics / nonlinear hyperbolic systems / smooth solution / steady-state solution / large scale practical applications / numerical solution / energy / /
NaturalFeature
inlet Mach / /
Organization
School of Mathematics / HDG EDG / Department of Aeronautics / American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / Stanford University / Massachusetts Institute of Technology / American Institute of Aeronautics and Astronautics By / University of Minnesota / Minneapolis / Department of Aeronautics and Astronautics / Stanford / American Institute of Aeronautics and Astronautics As / /
Person
J. S. Hesthaven / E. M. Ronquist / Whk / /
Position
hb / Prime Minister / Professor / Scientist / integral Pm / /
Product
Newton-Raphson / /
ProgrammingLanguage
FL / K / /
ProvinceOrState
Texas / Minnesota / Florida / Hawaii / New York / California / Massachusetts / /
An Embedded Discontinuous Galerkin Method for the Compressible Euler and Navier-Stokes Equations