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 |