2020 - Member of the National Academy of Engineering For development and validation of computational models for high-fidelity simulation of supersonic and hypersonic interactions.
Graham V. Candler mainly investigates Mechanics, Hypersonic speed, Non-equilibrium thermodynamics, Computational fluid dynamics and Thermodynamics. His study in Mechanics is interdisciplinary in nature, drawing from both Optics and Classical mechanics. His Hypersonic speed study is concerned with the larger field of Aerospace engineering.
His work deals with themes such as Computational physics, Diatomic molecule, Dissociation, Atomic physics and Stagnation point, which intersect with Non-equilibrium thermodynamics. The concepts of his Computational fluid dynamics study are interwoven with issues in Double wedge, Perfect gas and Wedge. His research in Boundary layer intersects with topics in Turbulence, Reynolds number, Mach number and Wind tunnel.
His scientific interests lie mostly in Mechanics, Hypersonic speed, Computational fluid dynamics, Boundary layer and Mach number. He regularly ties together related areas like Classical mechanics in his Mechanics studies. The Hypersonic speed study combines topics in areas such as Flow, Non-equilibrium thermodynamics, Inviscid flow and Shock wave.
His work in Non-equilibrium thermodynamics addresses subjects such as Atomic physics, which are connected to disciplines such as Dissociation. Computational fluid dynamics is closely attributed to Flow in his study. His studies deal with areas such as Freestream and Optics as well as Mach number.
His primary scientific interests are in Mechanics, Hypersonic speed, Boundary layer, Mach number and Computational fluid dynamics. His study in Mechanics focuses on Laminar flow, Direct numerical simulation, Flow, Reynolds number and Computer simulation. His work carried out in the field of Laminar flow brings together such families of science as Inflow and Shock.
His Hypersonic speed study deals with the bigger picture of Aerospace engineering. As a member of one scientific family, Graham V. Candler mostly works in the field of Boundary layer, focusing on Turbulence and, on occasion, Baroclinity. In his research, Large eddy simulation is intimately related to Supersonic speed, which falls under the overarching field of Computational fluid dynamics.
Mechanics, Hypersonic speed, Computational fluid dynamics, Aerospace engineering and Boundary layer are his primary areas of study. Graham V. Candler brings together Mechanics and Cone to produce work in his papers. His Hypersonic speed research includes themes of Reynolds-averaged Navier–Stokes equations, Turbulence, Freestream, Computation and Nose cone.
His research integrates issues of Non-equilibrium thermodynamics, Compressible flow and Supersonic speed in his study of Computational fluid dynamics. The various areas that he examines in his Boundary layer study include Oblique shock, Laminar flow, Instability, Geometry and Flow. His biological study spans a wide range of topics, including Rotational energy and Chemical kinetics.
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Review of Chemical-Kinetic Problems of Future NASA Missions, II: Mars Entries
Chul Park;John T. Howe;Richard L. Jaffe;Graham V. Candler.
Journal of Thermophysics and Heat Transfer (1993)
Data-Parallel Line Relaxation Method for the Navier -Stokes Equations
Michael J. Wright;Graham V. Candler;Deepak Bose;Deepak Bose.
AIAA Journal (1998)
The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation
Robert W. MacCormack;Graham V. Candler.
Computers & Fluids (1989)
Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium
Graham V. Candler;Robert W. MacCormack.
Journal of Thermophysics and Heat Transfer (1991)
Predicting failure of the continuum fluid equations in transitional hypersonic flows
Iain D. Boyd;Gang Chen;Graham V. Candler.
Physics of Fluids (1995)
Subgrid-Scale Models for Compressible Large-Eddy Simulations ?
M. Pino Martín;Ugo Piomelli;Graham V. Candler.
Theoretical and Computational Fluid Dynamics (2000)
A fully discrete, kinetic energy consistent finite-volume scheme for compressible flows
Pramod K. Subbareddy;Graham V. Candler.
Journal of Computational Physics (2009)
Thermal rate constants of the N 2 +O→NO+N reaction using ab initio 3 A″ and 3 A' potential energy surfaces
Deepak Bose;Graham V. Candler.
Journal of Chemical Physics (1996)
Hypersonic Boundary Layer Stability Analysis Using PSE-Chem
Heath B. Johnson;Graham V. Candler.
35th AIAA Fluid Dynamics Conference and Exhibit (2005)
The computation of hypersonic ionized flows in chemical and thermal nonequlibrium
Robert W. Maccormack;Graham V. Candler.
26th AIAA Aerospace Sciences Meeting (1988)
University of Colorado Boulder
University of Southern California
California Institute of Technology
California Institute of Technology
University of Minnesota
Purdue University West Lafayette
Norwegian University of Science and Technology
Queen's University
Princeton University
University of Minnesota
Profile was last updated on December 6th, 2021.
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