![]() 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
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