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ELORET's computational fluids researchers have worked and published extensively in direct support of several NASA and Industry programs. They have developed and utilized many advanced CFD codes and models for a broad range of applications. Expertise and help are available in the following:

Applications

• separating boundary layers
• shear layers and recovering flows
• reacting flows
• highly ionized flows
• wakes, jets, and plumes
• three-dimensional unsteady flows
• thermochemical non-equilibrium flows
• rarefied flows
• airfoils, wings, and rotors
• inlets and nozzles
• hypersonic single- and multi-body rockets, blunt bodies
• high lift systems

Codes

• 3D Reynolds averaged Navier Stokes (RANS)
• boundary layer
• inviscid
• 3D unsteady
• rarefied (DSMC and free molecular)
• large eddy simulation (LES)
• direct numerical simulation (DNS)

Turbulence Models

• algebraic (Baldwin-Lomax, Johnson-King, . . .)
• field equation (Spalart, Jones-Launder, . . .)
• full Reynolds stress (Wilcox, . . .)
• renormalization group theory (Yakhot-Orzag)
• shear stress transport (Menter)

Thermochemical Models

• thermochemical non-equilibrium (Park's 2 Temperature, . . .)