TALK KEYWORD INDEX
This page contains an index consisting of author-provided keywords.
| $ | |
| $\gamma$-$Re_\theta$ SST transition model | |
| 1 | |
| 1.Partially Rigidized Parachute (PRP) | |
| 2 | |
| 2.Surrogate models | |
| 3 | |
| 3.Artificial Neural Networks (ANN) | |
| 4 | |
| 4.Multi-Objective and Multidisciplinary Design Optimization (M2DO) | |
| 5 | |
| 5.Latin Hypercube Sampling (LHS) | |
| 6 | |
| 6.Design Domain analysis | |
| A | |
| A Mach 3 wind tunnel with a step | |
| ACFD | |
| Acoustic | |
| Acoustic modes | |
| Acoustic Pressure | |
| ACTFlow | |
| Active control method | |
| Active transition control | |
| AD | |
| Adiabatic flat plate | |
| Aerial spray | |
| Aero-elastic | |
| Aero-thermal | |
| Aeroacoustics | |
| Aerodynamic analysis | |
| Aerodynamic center | |
| aerodynamic coefficients | |
| Aerodynamic forces | |
| Aerodynamics | |
| Aeroengine Combustor | |
| Aerospike Nozzle | |
| Age of air | |
| AI | |
| air breathing propulsion | |
| Air Intake Drag | |
| Airborne disease transmission | |
| Airbrake | |
| Aircraft | |
| Aircraft design | |
| Aircraft Icing | |
| Aircraft Plume | |
| Aircraft Safety | |
| Aircraft valves | |
| Aircraft wake | |
| Airflow design | |
| Airfoil | |
| Algorithms | |
| ALM | |
| alternating injection | |
| Angle of Attack | |
| Anisotropic Minimum Dissipation | |
| ANN | |
| ANSYS | |
| ANSYS Fluent | |
| AoA | |
| AoA vane | |
| AoS | |
| artificial compressibility | |
| Artificial Neural Network | |
| Aspect ratio | |
| Atmospheric boundary layer | |
| Atomization | |
| AUSM | |
| AUSM+-up | |
| Automatic Structured Meshing | |
| Automobile | |
| Autorotation | |
| Axisymmetric Solver | |
| B | |
| BCC | |
| Bileaflet Mechanical Heart Valves | |
| BIREconcept | |
| Blackout | |
| Blade Element Method (BEM) | |
| Blast tube | |
| Blast Wave | |
| Bluff bodies | |
| Boundary conditions on electric potential Continuity errors in current density and magnetic field | |
| Boundary Layer | |
| Boundary Layer control | |
| Bubble cluster | |
| Buffet forcing function | |
| Building-Cube Method | |
| Bulk viscosity | |
| Bulk Viscosity ACM | |
| Buoyancy | |
| Buoyant Vortex Dipole | |
| Bypass transition | |
| C | |
| Can-combustor | |
| Canard | |
| Canard wing body | |
| Carbuncle | |
| Cavitation number | |
| Centrifugal blood pumps | |
| Centrifugal force | |
| Certification | |
| CFD | |
| CFD Automation | |
| CFD simulation | |
| CFD study of Realistic car model | |
| CFD trends | |
| CFD++ | |
| CFD-DEM | |
| Channel flow | |
| clean energy | |
| CLSVOF | |
| CMM | |
| Co-rotating vortex generators | |
| Coalescence | |
| Compact schemes | |
| Compressibility | |
| Compressibility Effect | |
| Compressible | |
| Compressible boundary layer | |
| Compressible flows | |
| Compressible Navier Stokes | |
| Compressible Navier-Stokes equations | |
| Compressible ring vortex | |
| Computational aeroacoustics | |
| Computational Fluid Dynamics | |
| Computational Fluid Structure Acoustic Interaction | |
| Computational performance | |
| condition number | |
| Confinement | |
| Conjugate heat transfer | |
| Contact-line motion | |
| control surface | |
| convection-diffusion equation | |
| Convective heat transfer coefficient | |
| Convergence | |
| Convergence acceleration | |
| Corner separation | |
| Counter rotating vortex generators | |
| Crew module RCS thruster | |
| Cross Vane Diffuser | |
| Cross wind | |
| Crow instability | |
| CSD-CFD coupling | |
| CUDA C | |
| Current-driven MHD | |
| Cylinder | |
| D | |
| Data-Driven CFD | |
| dbnsTurbFoam | |
| Deep Learning | |
| Deflagration | |
| Deformation | |
| Deforming mesh | |
| Delta wing | |
| Density | |
| density driven flow | |
| DES | |
| Design | |
| Detached eddy simulation | |
| DG | |
| Diameter of cylinder | |
| Diatomic gases | |
| Diffuser position | |
| Dimple | |
| dimpled cylinder | |
| dimples | |
| Direct Flux Reconstruction | |
| Direct Numerical Simulation | |
| Direct simulation Monte Carlo (DSMC) | |
| Discontinuous Galerkin | |
| Discontinuous Galerkin method | |
| discrete adjoint method | |
| Discrete adjoints | |
| Discrete element method (DEM) | |
| Discrete Phase Model | |
| dissipation control | |
| DMD | |
| DNS | |
| Double Mach reflection | |
| Drag | |
| Drag coefficient | |
| Drag count | |
| drag crisis | |
| drag reduction | |
| Drag rise | |
| Drag sensitivity | |
| DrivAer model | |
| Droplet collision | |
| Droplet dispersion | |
| Droplet impact | |
| Droplet statistics | |
| DSMC | |
| Dusty gas flows | |
| Dynamic Distortion | |
| Dynamic Mesh | |
| Dynamic mode decomposition | |
| dynamic SGS models | |
| E | |
| EDC (Eddy Dissipation Concept) | |
| Eddy dissipation concept model | |
| Eddy Dissipation Model | |
| Efficiency | |
| ejector nozzle | |
| ELBM | |
| Electro-vortex flow | |
| Enstrophy production | |
| Entropy Damped AC | |
| Environmental control chamber | |
| EOR | |
| Ethylene | |
| Ethylene Combustion | |
| Euler Equations | |
| Euler solver | |
| Euler-Bernoulli modes | |
| Euler-Lagrangian Coupling | |
| Eulerian velocity correction method | |
| Evaporation | |
| expanded turbulent channel flow | |
| Experimental validation | |
| External Store | |
| F | |
| Fast Fourier Transform | |
| FDA benchmark | |
| Fighter aircraft | |
| fingering instability | |
| finite element method | |
| Finite volume method | |
| Finite Volume Solver | |
| Finite wing | |
| flapping wing | |
| Flapping Wing Aerodynamics | |
| Flexible channel | |
| flexible plume | |
| flexible wing | |
| float | |
| Flow asymmetry | |
| Flow control | |
| flow energy converter | |
| Flow instability | |
| Flow quality | |
| Flow Reconstruction | |
| Flow separation | |
| Flow-induced vibration | |
| Fluent | |
| Fluid structure interaction | |
| Fortran | |
| Friction model | |
| Friedlander's Curve | |
| Frisbee | |
| FSI | |
| full factorial sampling | |
| FV | |
| G | |
| Gaganyaan | |
| Gas turbines | |
| general pressure equation | |
| generative adversarial networks | |
| Genetic Algorithm | |
| Geometric nonlinearity | |
| Geometry Optimization | |
| Gerlach Shaping | |
| ghost points | |
| GPU | |
| GPU programming | |
| GPU-accelerated computing | |
| Granular | |
| Green-Gauss | |
| Grid fin | |
| GridPro | |
| Ground Effect | |
| Ground height to wing span ratio | |
| H | |
| Hammerhead launch vehicle | |
| Harris Hawks Optimization | |
| HARUAV | |
| Heat Flux | |
| Heat pipe | |
| Heat Transfer | |
| Helmholtz equation | |
| HiFUN | |
| High aspect ratio | |
| High aspect ratio wing | |
| High order methods | |
| High-order methods | |
| High-resolution | |
| High-speed | |
| higher order accuracy | |
| Higher-order methods | |
| Hinge momnet | |
| HLL-CPS scheme | |
| HPC | |
| HPT | |
| Human spaceflight | |
| Hybrid RANS/LES | |
| Hydrodynamic splitting | |
| Hydrogen Explosion | |
| Hypersonic | |
| Hypersonic boundary layer transition control | |
| Hypersonic Flow | |
| HySEA | |
| I | |
| Ice Accretion | |
| Ice protection system | |
| Icing | |
| Immersed boundary method | |
| Immersed boundary method (IBM) | |
| Impeller diameter | |
| Implicit | |
| Implicit Gradient Reconstruction | |
| In-board up | |
| Incompressible flow | |
| Infection Risk modeling | |
| Infinitely Fast Chemistry | |
| Infrared | |
| Injection | |
| Innovations | |
| Instability | |
| instability fingers | |
| internal flow | |
| Internal flows | |
| Internal hydraulics | |
| inverse Magnus effect | |
| ISRO | |
| J | |
| Jacobian | |
| Jet mixing | |
| Jet Plume | |
| Jets | |
| K | |
| k-ε model | |
| KEEP | |
| Kingery-Bulmash Equation | |
| Klystron effect | |
| L | |
| L/D ratio | |
| Lagrangian | |
| Lagrangian particle tracking | |
| Lamb Dipole | |
| Laminar flows | |
| laminar separation bubble | |
| Landing gear | |
| Large Eddy Simulation | |
| Large eddy simulations | |
| Large-eddy simulation | |
| Laser-fluid interaction | |
| Lattice Boltzmann Method | |
| Lattice fin | |
| Launch vehicle | |
| leading edge separation | |
| Legion | |
| LES | |
| Level-set method | |
| Lift | |
| Lift coefficient | |
| lift generation | |
| Lifting Line Theory | |
| Line replacement unit | |
| Line-Based techniques | |
| Linear Stability Theory | |
| Liquid jet in crossflow | |
| Liquid methane | |
| Liquid propellants | |
| Localised Artificial Diffusivity | |
| lock-in | |
| Long bubble | |
| Low Dissipation | |
| Low frequency unsteadiness | |
| low Mach number | |
| Low Reynolds number | |
| Low Reynolds number flow | |
| LPT | |
| LS-DYNA | |
| LSFD-U | |
| LSKUM | |
| Lunar landing | |
| M | |
| M219 cavity | |
| Mach 80 astrophysical jet | |
| Mach number | |
| Machine Learning | |
| Machine Learning | |
| Magnetohydrodynamic flow | |
| Magnus effect | |
| Mass Transfer | |
| maximum lift coefficient | |
| MDO | |
| Mesh adaptation | |
| Mesh Adaption | |
| Mesh-Free | |
| Meshfree | |
| Meshfree LSKUM | |
| Meshing | |
| meshless | |
| Methane oxygen | |
| Metric-field | |
| MHD | |
| Micro Gas Turbines Centrifugal Compressor | |
| Microchannels | |
| Minkowski functionals | |
| Missile | |
| Missile fin | |
| missile plume | |
| Missiles | |
| mixing | |
| ML | |
| Mode multigrid | |
| Mode-Staging | |
| Modified Kinematics | |
| Modified γ-model | |
| Modulated Gradient Model | |
| Morphology | |
| Moving body simulations | |
| moving boundary | |
| moving mesh | |
| Moving shock wave | |
| MPI | |
| Multi-block-multi-mesh | |
| Multi-Element Airfoils | |
| Multi-physics | |
| Multiphase | |
| Multiphase Flow | |
| N | |
| NACA0012 | |
| NAL | |
| Natural convection | |
| Naturally generated vortex ring | |
| Navier-Stokes equations | |
| Near stall | |
| Neural Network | |
| Newtonian flow | |
| noise prediction | |
| Non-Equilibrium Flows | |
| Non-Newtonian flow | |
| Nose Bluntness | |
| Nozzle overexpansion | |
| nozzle pressure ratio | |
| Number of blades | |
| numerical methods | |
| Numerical modelling | |
| Numerical simulation | |
| Numerical Study | |
| O | |
| OASPL | |
| Oberbeck-Boussinesq Approximation | |
| OMAR 5 airfoil | |
| One Inlet and One Outlet Model | |
| open cavity flow | |
| Open-source | |
| Open-source software | |
| OpenACC | |
| OpenFOAM | |
| OpenMP | |
| Optimal perturbation | |
| Optimal sensor locations | |
| Optimisation | |
| Optimization | |
| Overpressure | |
| overset mesh | |
| P | |
| Palinstrophy production | |
| Parachute | |
| parallel computational fluids dynamics | |
| Parallel programming | |
| Parallelization | |
| PARANAM solver | |
| Partial Differential Equations | |
| Particle | |
| Particle laden compressible flow | |
| Particle-laden | |
| Particle-Laden Flow | |
| Passive flow control | |
| Path flux analysis | |
| Performance analysis | |
| Perturbation | |
| Physics-Informed Neural Network | |
| PINNs | |
| Pivot location | |
| Plug Nozzle | |
| plume ingestion | |
| plume interaction | |
| plume path | |
| Plunging Airfoil | |
| Point particle method | |
| Poisson | |
| Polyatomic gases | |
| Polycyclic aromatic hydrocarbons | |
| Pope’s correction | |
| Pore-scale simulation | |
| Porosity/Distributed Resistance | |
| Porous | |
| porous medium | |
| Positivity Condition | |
| Positivity-preservation | |
| Potential Flow | |
| power-law fluid | |
| PRAVAHA | |
| Premixed combustion | |
| Pressure | |
| Pressure Based Solver | |
| Pressure coefficients | |
| Pressure Feedback Technique | |
| Pressure Gradient | |
| Pressure Recovery | |
| pressure-reducing and the shutoff valve | |
| PRF | |
| primary nozzle | |
| Propeller | |
| Proper Orthogonal Decomposition | |
| Prosthetic Heart Valves | |
| Pseudo-Spectral Method | |
| Pump as Turbine | |
| pylon | |
| Q | |
| Quantum computing | |
| R | |
| RAE S-duct | |
| RANS | |
| Re-entry | |
| Reacting flow | |
| reattachment | |
| recirculation | |
| recovery | |
| rectangular cavity | |
| Reduced Order Modeling | |
| REEF3D | |
| Reentry | |
| Regent | |
| Reinforcement Learning | |
| Relaminarization | |
| resonant peaks | |
| Restart | |
| Reynolds Averaged Navier Stokes | |
| Reynolds Stress Model | |
| Riemann Solver | |
| Rigid plume | |
| Rocket combustion | |
| Rocket nozzle | |
| Roe-type Riemann solver | |
| Roll moment | |
| Rossiter Mode | |
| Rotating cylinder | |
| Roughness | |
| Rudimentary | |
| S | |
| S-duct | |
| S-shaped | |
| SA | |
| Sandia D flame | |
| SBLI | |
| Scheme | |
| School classroom | |
| Scientific Computing | |
| Scramjet | |
| Scramjet Intake | |
| scramjet vehicle | |
| Screech | |
| secondary vortex | |
| self-propulsive force | |
| self-supervised | |
| Sense of rotation | |
| Separated flows | |
| Separation | |
| Separation bubble | |
| Separation dynamics | |
| Serpentine air intake duct | |
| Serpentine Inlet | |
| SGS | |
| shape sensitivites | |
| Sharkskin denticle | |
| Shear stress and shear rate | |
| Shock | |
| Shock boundary layer interaction | |
| Shock capturing | |
| Shock Diamonds | |
| Shock induced flow separation | |
| Shock Tube | |
| Shock wave boundary layer Interaction | |
| Shock wave in an enclosure | |
| Shock wave-boundary layer interaction | |
| shock-capturing | |
| Shock-particle interaction | |
| Short bubble | |
| Side force | |
| Sideslip | |
| Sigma | |
| Simulation Driven Design | |
| Solver | |
| Sound Pressure Level | |
| Space | |
| Spalart-Allmaras model | |
| Spanwise length | |
| Spectral analysis | |
| Spectral method | |
| speedup | |
| Spillage | |
| SPL | |
| Splitter Plate | |
| Sports | |
| Square Elbow | |
| Stability | |
| Stability derivatives | |
| Stall | |
| static port | |
| Static structural solver | |
| Stator | |
| stencil | |
| Stoke's hypothesis | |
| Store Separation | |
| SU2 | |
| Sub-grid scale combustion models | |
| Subcritical LOX jet | |
| submerged intake | |
| subsonic flow | |
| Suction | |
| Suction effect | |
| Suction-blowing excitation | |
| SUP | |
| super-resolution | |
| Superhydrophobic microchannels | |
| Supersonic | |
| Supersonic base flows | |
| Supersonic Combustion | |
| supersonic flow | |
| supersonic speeds | |
| Surface heterogeneity | |
| Surface tension | |
| Surrogate Model | |
| Suspension | |
| SWBLI | |
| Swirling round jets | |
| SWTBLI | |
| T | |
| Tailless aircrafts | |
| TBCC | |
| TBD1 | |
| TBD2 | |
| TBD3 | |
| Thermal blooming | |
| Thermo-elastic | |
| Throttle Dependent Drag | |
| TPMS lattice | |
| Transient jet | |
| Transition | |
| Transition model | |
| Transition onset | |
| Transonic Axial compressor | |
| Transonic Flow | |
| Transonic Flows | |
| Transonic speeds | |
| Transpiration Boundary Condition | |
| Transport aircraft | |
| Trapezoidal vortex generator | |
| turbomachinery | |
| Turbulence | |
| Turbulence Model | |
| Turbulence Modeling | |
| Turbulence modeling of flow separation | |
| Turbulence models | |
| Turbulence Prediction | |
| Turbulence structures | |
| Turbulent | |
| Turbulent channel flow | |
| Turbulent flow | |
| Two Inlet and Two Outlet model | |
| Two stage rocket Scramjet | |
| Two-phase flow | |
| two-phase flows | |
| Two-phase fluid flow | |
| U | |
| unconventional | |
| Unified Formulation | |
| Unstart | |
| Unsteady | |
| unsteady flow | |
| Unsteady flow analysis | |
| Unsteady Flows | |
| Unsteady Panel Method | |
| Unsteady pressure field | |
| Unstructured grid | |
| URANS | |
| V | |
| validation | |
| Vaneless Diffuser | |
| VAWT | |
| Vehicle | |
| Vehicle Aerodynamics | |
| Velocity | |
| Velocity Profile | |
| Venkatakrishnan limiter | |
| Ventilation | |
| VOF | |
| Vogel-Escudier Flow | |
| Void wave | |
| Volume of fluid | |
| Volume of fluid method | |
| volume-of-fluid | |
| Vortex dipole impingement | |
| vortex interactions | |
| Vortex rebound | |
| Vortex ring shock wave interaction | |
| Vortex shedding | |
| Vortex-induced vibration | |
| W | |
| Wake effects | |
| wake induced vibrations | |
| Wake transition | |
| Wall dominated flows | |
| wall function | |
| wall-modeled large-eddy simulation | |
| Weapon bay cavity | |
| Wedge | |
| Weighted Least Square | |
| weighted least-squares | |
| Wind farm | |
| Wind flow direction | |
| Wind Flow models | |
| Wind tunnel | |
| wind tunnel test | |
| Wing | |
| Wing Design | |
| Winglet | |
| Wingtip | |
| WM-LES | |
| Y | |
| Y Intake | |
| Yaw misalignment | |
| Yawing moment | |
| ∆ | |
| ∆y/D | |