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Unstructured Grid
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1999 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 1
A Code for Shape Generation and Aerodynamic Design of Aircraft
A Comparative Aerodynamic Investigation of a 20° SAE Notchback Model
Adaptive Determination of the Optimal Exchange Location in Wall-Modeled Large-Eddy Simulation
Adaptive unstrukturierte Netze zur numerischen Simulation von Strömungsvorgängen in Turbomaschinen
A Design Method for Three-Dimensional Scramjet Nozzles with Shape Transition
Aeronautical CFD in the age of Petaflops-scale computing: From unstructured to Cartesian meshes
Aircraft Performance of Kenyalang Fuel Cell UAV
Analysis of a Cylindrical Specimen Heated by an Impinging Hot Hydrogen Jet
An inverse design method for engine nacelles and wings
A non-linear finite element method on unstructured meshes for added resistance in waves
An Overview of Ares-I CFD Ascent Aerodynamic Data Development and Analysis Based on USM3D
Application of a Discontinuous Galerkin Method to Discretize Acoustic Perturbation Equations
Application of a Riemann Solver Unstructured Finite Volume Method to Combustion Instabilities
Application of New Absorbing Boundary Condition with Finite Volume Schemes
Application of the FUN3D Solver to the 4th AIAA Drag Prediction Workshop
Approximate Method for Computing Convective Heating on Hypersonic Vehicles Using Unstructured Grids
Automated Mesh Generation and Solution Analysis of Arbitrary Airfoil Geometries
Automatic Embedding of Potential Flow Wake Surfaces in Generic Monolithic Unstructured Meshes
Base Heating Environment During Ground Testing of a Lunar Lander Demonstrator
Boundary-Layer Stability Analysis of the Mean Flows Obtained Using Unstructured Grids
CFD Analysis of Flapping Wing for MICAV Application
Comparison of Computational Fluid Dynamics Hover Predictions on the S-76 Rotor
Comparison of Finite-Volume and Methods for Large-Eddy Simulation of Combustor Port Flow
Comparison of Simulated Sonic Boom in Stratified Atmosphere with Flight Test Measurements
Computations from the Fourth Drag Prediction Workshop Using the Edge Solver
Computations of High-Lift Wing Configuration on Unstructured Grids Using Models
Constrained Hermite Interpolation for Mesh-Free Derivative Estimation Near and On Boundaries
Convergence Analysis of Shock-Capturing and Shock-Fitting Solutions on Unstructured Grids
Convergence Study of Local Continuum Sensitivity Method Using Spatial Gradient Reconstruction
Critical Study of Agglomerated Multigrid Methods for Diffusion
Curved Boundary Treatments for the Discontinuous Galerkin Method Applied to Aeroacoustic Propagation
Deformable Overset Grid for Multibody Unsteady Flow Simulation
Development of an Aeroelastic Modeling Capability for Transient Nozzle Flow Analysis
Development of Vertex-Centered High-Order Schemes and Implementation in FUN3D