Various 2D Adjoint-Based Airfoil Designs.

Unsteady Space Shuttle Cable Tray Analysis.

Adjoint-Based Adaptation for 3D Sonic Boom.

Biologically-Inspired Morphing Aircraft.

Line Construction for Line-Implicit Relaxation.

Mach 24 Temperature-Based Adaptation of Space Shuttle Configuration in Chemical Nonequilibrium.

Adjoint-Based Adaptation Applied to Supersonic Double-Airfoil.

Adjoint-Based Adaptation Applied to High-Lift Airfoil.

Adjoint-Based Adaptation Applied to AIAA DPW II Wing-Body.

Time-Dependent Oscillating Flap Demonstration.

Dynamic Overset Grid Demonstration Using A Simple Rotor/Fuselage Model.

DES ground wind simulation on ARES configuration.

FUN3D and LAURA v5 STS-2 heating comparisons.

Design of F-15 with Simulated Aeroelastic Effects.

Ongoing Improvements in Computational Performance.

Smart Truck Simulations at BMI Corporation.Flight Trajectories for Various Rocket Geometries.More Smart Truck Simulations at BMI Corporation.Computational vs Experimental Schlieren for Supersonic Retro-Propulsion.Computational Schlieren for Unsteady Simulation of Launch Abort System.Mesh adaptation for RANS simulation of supersonic business jet.Time-dependent discrete adjoint solution for UH60 helicopter in forward flight.Computational Schlierens for Supersonic Retro-Propulsion.Notional unducted engine with counter-rotating blades.Simulation of biologically-inspired flapping wing.Forward and adjoint solutions for aeroelastic F-15.

Forward and adjoint solutions for wind turbine.Updated scaling study on ORNL Cray XK7 system.Max L/D for steady flow over a wing-body-tail using Sculptor.Max L/D over a pitching cycle for a wing.Lift-constrained drag minimization for DPW wing.Max L/D for steady flow at two different Mach numbers.

Merge VGRID mesh into mixed elements and run solution.Site Contents Software Overview and References

How to divide two variables in tecplot