Keywords: جریان فیزیکی; Body and wing; Flow field; Hypersonic flow; Shock/shock interaction; Wave configurations;
مقالات ISI جریان فیزیکی (ترجمه نشده)
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Keywords: جریان فیزیکی; Spaceplane; Hypersonic flow; Non-equilibrium flow; Aerodynamics; CFD;
Keywords: جریان فیزیکی; Hypersonic flow; Forward facing cavity; Oscillation period; Shock standoff; Unsteady heat flux; Schlieren visualisation;
Keywords: جریان فیزیکی; Hypersonic flow; Thermochemical nonequilibrium; Vibration-dissociation coupling; Shock-wave/boundary-layer interaction;
Keywords: جریان فیزیکی; Heat transfer; Hypersonic flow; Thermal nonequilibrium; Chemical kinetic model; Governing temperature;
Keywords: جریان فیزیکی; Burnett equations; Linearized stability; Hypersonic flow;
Keywords: جریان فیزیکی; Computational fluid dynamics; Residual distribution schemes; Hypersonic flow; Entropy variables; Thermo-chemical non-equilibrium; Unstructured grids;
Keywords: جریان فیزیکی; Hypersonic flow; Lateral jet interaction; Wind tunnel; Schlieren visualization; Pressure;
Keywords: جریان فیزیکی; Computational fluid dynamics; Scramjet nozzle; Hypersonic flow; Energy addition; Variance analysis;
Keywords: جریان فیزیکی; Truncated cone; Pressure-sensitive paint; Hypersonic flow;
Keywords: جریان فیزیکی; Computational fluid dynamics; Scramjet nozzle; Hypersonic flow; Energy deposition; Optimization design;
Keywords: جریان فیزیکی; Hypersonic flow; Drag and heat reduction; Forward-facing cavity; Opposing jet; Jet operating conditions; Freestream angle of attack; Physical dimensions;
Keywords: جریان فیزیکی; Hypersonic flow; Waverider; Variable; Blunt leading edge;
Keywords: جریان فیزیکی; Chemical reactions; Compressible flows; Fluid dynamics; Finite volume methods; Hypersonic flow; Navier–Stokes equations; Numerical method
Keywords: جریان فیزیکی; Computational fluid dynamics; Hypersonic flow; Shock-wave-boundary layer interaction; Shock-shock interaction; Reacting flow;
Keywords: جریان فیزیکی; Hypersonic flow; Plasma sheath; Ablation; Electromagnetic scattering characteristic; Numerical simulation
Keywords: جریان فیزیکی; Co-axial thermocouple; Shock tunnel; Hypersonic flow; Fay-Riddell; Stagnation point heat flux; Base heat flux;
Keywords: جریان فیزیکی; ADC; Analog to Digital Converter; VSSC; Vikram Sarabhai Space Centre; MACOR®; trademark for a machinable glass ceramic developed and sold by Corning, Inc; K-type co-axial thermocouple; Fast response; Shock tunnel; Hypersonic flow; Fay-Riddell; Stagnati
Keywords: جریان فیزیکی; Carbuncle; Compressible flow; Hypersonic flow; Residual distribution; Finite volume; Artificial diffusion;
Keywords: جریان فیزیکی; Hypersonic flow; Drag and heat reduction; Forward-facing cavity; Counterflowing jet; Maximum thrust nozzle;
Keywords: جریان فیزیکی; Hypersonic flow; Plasma wind tunnel; UHTC;
Keywords: جریان فیزیکی; Aerodynamic performance; High temperature effect; Hypersonic flow; Thermochemical non-equilibrium; Waverider
Keywords: جریان فیزیکی; Quasi-classical trajectory method; Molecular oxygen; Ozone potential surface; Hypersonic flow; Vibrational relaxation; Exchange reaction;
Keywords: جریان فیزیکی; Hypersonic flow; Separation control; Shock–Boundary Layer Interaction (SBLI); Shock tunnel experiments
Keywords: جریان فیزیکی; Chromium; Numerical simulation; Reaction; Drag reduction; Hypersonic flow;
Shock capturing for discontinuous Galerkin methods with application to predicting heat transfer in hypersonic flows
Keywords: جریان فیزیکی; Discontinuous Galerkin method; Hypersonic flow; Shock capturing; Artificial viscosity; Heat transfer;
Sensitivity analysis of geometric parameters upon the aerothermodynamic performances of Mars entry vehicle
Keywords: جریان فیزیکی; Computational fluid dynamics; Mars Science Laboratory; Hypersonic flow; Aerothermodynamics; Sensitivity analysis;
Hypersonic shock wave transitional boundary layer interactions - A review
Keywords: جریان فیزیکی; Hypersonic flow; Shock wave boundary layer interaction; Transitional flow;
State-specific dissociation in O2-O2 collisions by quasiclassical trajectory method
Keywords: جریان فیزیکی; Quasiclassical trajectory method; Molecular oxygen; Tetraoxygen; Hypersonic flow; Vibrational relaxation;
Improved k-Ï-γ model for crossflow-induced transition prediction in hypersonic flow
Keywords: جریان فیزیکی; Hypersonic flow; Boundary layer transition; Transition model; Crossflow;
On transition of type V interaction in double-wedge flow with non-equilibrium effects
Keywords: جریان فیزیکی; Shock interaction; Non-equilibrium effects; Shock polar; Hypersonic flow;
Assessment of SLAU2 and other flux functions with slope limiters in hypersonic shock-interaction heating
Keywords: جریان فیزیکی; SLAU2; AUSM+-up; AUSMPW+; Flux limiter; Hypersonic flow
Parallel Navier–Stokes simulations for high speed compressible flow past arbitrary geometries using FLASH
Keywords: جریان فیزیکی; FLASH code; Navier–Stokes; Hypersonic flow; Parallel
Improved-Delayed-Detached-Eddy Simulation of cavity-induced transition in hypersonic boundary layer
Keywords: جریان فیزیکی; Hypersonic flow; Transition; Cavity; Improved-Delayed-Detached-Eddy Simulation (IDDES);
Centerline instabilities on the hypersonic international flight research experimentation HIFiRE-5 elliptic cone model
Keywords: جریان فیزیکی; Elliptic cone; Hypersonic flow; Linear modal instability; Spatial BiGlobal analysis;
Computation of 1-D shock structure in a gas in rotational non-equilibrium using a new set of simplified Burnett equations
Keywords: جریان فیزیکی; Burnett equations; Hypersonic flow; Shock structure; Rotational non-equilibrium
Modeling hypersonic entry with the fully-implicit Navier–Stokes (FIN-S) stabilized finite element flow solver
Keywords: جریان فیزیکی; Stabilized finite elements; Compressible flow; Hypersonic flow; Reentry; Surface ablation
Hypersonic interference heating on cones with short three-dimensional protuberances
Keywords: جریان فیزیکی; Hypersonic flow; Laminar boundary layer; Three-dimensional flow interference; Flow separation; Platinum thin-film gauges;
Laser-induced plasma ignition studies in a model scramjet engine
Keywords: جریان فیزیکی; Hypersonic flow; Supersonic combustion; Planar laser-induced fluorescence imaging; Plasma-assisted combustion; Laser-induced ignition; Laser-induced plasma
Investigation of thermal protection system by forward-facing cavity and opposing jet combinatorial configuration
Keywords: جریان فیزیکی; Aerodynamic heating; Forward-facing cavity; Hypersonic flow; Opposing jet; Thermal protection system
Numerical study of unsteady starting characteristics of a hypersonic inlet
Keywords: جریان فیزیکی; Hypersonic flow; Inlet; Scramjet; Start; Unsteady
Gradient-based methods for uncertainty quantification in hypersonic flows
Keywords: جریان فیزیکی; Uncertainty quantification; Adjoint methods; Gradient-based optimization; Hypersonic flow
Hypersonic environment assessment of the CIRA FTB-X re-entry vehicle
Keywords: جریان فیزیکی; Aerodynamics; Aerothermodynamics; Hypersonic flow; Preliminary design; Heat transfer; Re-entry vehicles
Transient analysis of counterflowing jet over highly blunt cone in hypersonic flow
Keywords: جریان فیزیکی; Transition; Hypersonic flow; Numerical analysis; Counterflowing jets
Pressure-sensitive paint on a truncated cone in hypersonic flow at incidences
Keywords: جریان فیزیکی; Pressure-sensitive paint; Hypersonic flow; Oil flow; Surface pressure mapping; Shock wave
An improved wavelength selection scheme for Monte Carlo solvers applied to hypersonic plasmas
Keywords: جریان فیزیکی; Monte Carlo methods; Hypersonic flow; Planetary entry; Hypersonic plasma radiation; Random number database; Line-by-line radiation;
Optimizations and OpenMP implementation for the direct simulation Monte Carlo method
Keywords: جریان فیزیکی; Direct simulation Monte Carlo; Hypersonic flow; OpenMP
Physico-chemical state of the air at the stagnation point during the atmospheric reentry of a spacecraft
Keywords: جریان فیزیکی; Chemical kinetic; Dissociation; Finite volumes; Frozen; Hypersonic flow; Non-equilibrium; Reactive flow; Supersonic flow; Vibration
Positivity-preserving flux-limited method for compressible fluid flow
Keywords: جریان فیزیکی; Positivity preservation; Compressible fluid; Monotonicity; Flux limiters; Flux vector splitting; Steger-Warming scheme; Hypersonic flow
Correcting lateral heat conduction effect in image-based heat flux measurements as an inverse problem
Keywords: جریان فیزیکی; Image-based heat flux measurement; Temperature sensitive paint; Lateral heat conduction; Integral equation; Deconvolution; Hypersonic flow;