Lars-Erik Eriksson
Showing 125 publications
Dynamics of flame extinction in narrow channels with cold walls: Heat loss vs acceleration
Elimination of Shock-Associated Noise in Supersonic Jets by Destructive Wave Interference
Elimination of shock associated noise in supersonic jets by destructive wave interference
Noise radiated by low-Reynolds number flows past a hemisphere at Ma=0.3
CFD analysis of a SGT-800 burner in a combustion RIG
Assessment of Flap Side-Edge Fence Noise using SNGR Method
Simulation of Tip-Clearance Effects in a Transonic Compressor
CFD investigation of a Stirling engine flexi-fuel burner based on MILD combustion
Aero-acoustic analysis and assessment of conceptual low-noise airframe configurations
CFD investigation of a Stirling engine f exi-fuel burner based on MILD combustion
Noise Control of Supersonic Jet with Steady and Flapping Fluidic Injection
CAA analysis of a wing section with flap side-edges based on hybrid RANS-LES computation
Numerical Simulation of Stirling Engines Using an Unsteady Quasi-One-Dimensional Approach
Numerical Validation of a Time Domain Perforated Plate Model with Nonlinear and Inertial Effects
Predictive Capability of CFD Models for Transonic Compressor Design
Surface integral analogy approaches for predicting noise from 3D high-lift low-noise wings
Investigation of Screech in Supersonic Jets Using Modal Decomposition
The Role of Nozzle Contour on Supersonic Jet Thrust and Acoustics
Near-field and far-field spectral analyzis of supersonic jet with and without fluidic injection
A Novel Solver Acceleration Technique Based on Dynamic Mode Decomposition
Investigation of supersonic jet flow using modal decomposition
Comparison of Eigenmode Extraction Techniques for Separated Nozzle Flows
Investigation of a Separated Nozzle Flow with Transonic Resonance Using Dynamic Mode Decomposition
Exploration of temperature effects on the far-field acoustic radiation from a supersonic jet
Analysis of Supersonic Jet Thrust with Fluidic Injection
Supersonic turbojet noise reduction
Supersonic Jet Excitation using Flapping Injection
Evaluation of global mechanisms for les analysis of SGT-100 DLE combustion system
A Comprehensive Investigation of Pulsed Fluidic Injection for Active Control of Supersonic Jet Noise
Quasi-steady stages in the process of premixed flame acceleration in narrow channels
Balancing efficiency and stability in the design of transonic compressor stages
SNGR Method for Assessing Noise Induced by Flap Side-Edges
The Response of Supersonic Jet Noise Components to Fluidic Injection Parameters
Influence of gas compression on flame acceleration in the early stage of burning in tubes
Supersonic Jet Noise Reduction Using Steady Injection and Flapping Injection
Nozzle throat optimization for supersonic jet noise reduction
Local flow properties in relation to noise generation for low-noise high-lift configurations
CFD optimization of a transonic compressor using multiobjective GA and metamodels
Active Suppression of Supersonic Jet Noise Using Pulsating Micro-Jets
Design of compressor blades considering efficiency and stability using CFD based optimization
Aeroacoustic Assessment of Conceptual Low-Noise High-Lift Wing Configurations
Experimental and Numerical Investigation of a Supersonic Convergent-Divergent Nozzle
Techniques for supersonic turbojet noise reduction
Nozzle Throat Optimization on Acoustics and Performance of a Supersonic Jet
Assessment of high-lift concepts for a regional aircraft in the ALONOCO project
A Four-Step Global Reaction Mechanism for CFD Simulations of Flexi-Fuel Burner for Gas Turbines
CFD validation of a high speed transonic 3.5 stage axial compressor
CFD INVESTIGATION OF SWIRL-STABILIZED FLEXI-FUEL BURNER USING METHANE-AIR MIXTURE FOR GAS TURBINES
Evaluation of Optimized 3-step Global Reaction Mechanism for CFD Simulations on Sandia Flame D
Optimized Global Mechanisms for CFD Analysis of Swirl-Stabilized Syngas Burner for Gas Turbines
Large Eddy Simulation of premixed flames with multi-step global reaction mechanisms
LIMITATIONS ON TUBE FILLING IN A PULSED DETONATION ENGINE
TIME-DOMAIN MODELING OF SCREECH-DAMPING LINERS IN COMBUSTORS AND AFTERBURNER
Absorbing Inlet Boundary Analysis of Rotor Wake/Stator Time Domain Computations
Micro-Jet Flow Control for Noise Reduction of a Supersonic Jet from a Practical C-D Nozzle
Investigation of large scale shock movement in transonic flow
Experimental and Numerical Investigation of a Novel Acoustic Liner Concept
Flame acceleration in channels with obstacles in the deflagration-to-detonation transition
Aeroacoustics and Performance Modeling of a Counter-Rotating Propfan
Analysis of flame acceleration induced by wall friction in open tubes
Near-Field Jet Noise from a Supersonic C-D Chevron Nozzle
Forward Flight Effects on the Shock Structure From a Chevron C-D Nozzle
Comparison of Flow Control Methods Applied to Conical C-D Nozzles
Analysis of thermo-acoustic properties of combustors and Afterburners
Experimental and Numerical Investigation of a Supersonic C-D Nozzle
An Absorbing Inlet Buffer Layer for Rotor Wake/Stator Time Domain Computations
Different stages of flame acceleration from slow burning to Chapman-Jouguet deflagration
Rotor Wake/Stator Broadband Noise Calculations Using Hybrid RANS/LES and Chorochronic Buffer Zones
Mechanism of fast flame acceleration in cylindrical tubes with obstacles
LARGE EDDY SIMULATION OF A LEAN PREMIXED LOW SWIRL BURNER
Experimental and Numerical Investigation of a Supersonic C-D Chevron Nozzle
Supersonic Jet Noise from a Conical C-D Nozzle with Forward Flight Effects
Validation of a Time- and Frequency-Domain Grazing Flow Acoustic Liner Model
Computational Study of Mixed Hydrodynamic-Acoustic Waves in Gas Turbine Afterburner Flows
Physical Mechanism of Ultrafast Flame Acceleration
FLOW-FLAME INTERACTIONS IN A LEAN PREMIXED LOW SWIRL BURNER
Validation of a Time & Frequency Domain Grazing Flow Acoustic Liner Model
Design of an Aggressive Flow-controlled Turbine Duct
Flow-flame interaction in a closed chamber
Bubble velocity in the nonlinear Rayleigh-Taylor instability at a deflagration front
Non-axisymmetric Endwall Shape Optimization of an Intermediate Turbine Duct
The Rayleigh-Taylor instability in inertial fusion, astrophysical plasma and flames
Evaluation of Nonlinear Rotor Wake/Stator Interaction by using Time Domain Chorochronic Solver
Nonlinear Rotor Wake/Stator Interaction Computations
Numerical study of turbulent flame velocity
Flame acceleration in the early stages of burning in tubes
Flame-sound interaction in tubes with nonslip walls
Flow and noise predictions for a mixer-ejector engine configuration using LES
Large Eddy Simulation of Transonic Flow with Shock Wave/Turbulent Boundary Layer Interaction
Flame propagation along the vortex axis
LES based jet noise prediction for mixer-ejector configurations including acoustic liner model
Response Surface-based Transition Duct Shape Optimization
Intermediate Turbine Duct Design and Optimization
A Tuning-free Body-force Vortex Generator Model
Accelerating flames in cylindrical tubes with nonslip at the walls
Violent folding of a flame front in a flame-acoustic resonance
Flame oscillations in tubes with nonslip at the walls
Effects of Inflow Conditions and Subgrid Model on LES for Turbulent Jets
Evaluation of modeled deterministic stress terms and thier effects in a 3D transonic compressor
LES Prediction of Flow and Acoustic Field of a Coaxial Jet
Large-Eddy Simulation of Subsonic Turbulent Jets and Their Radiated Sound
Acoustic Source Terms for the Linearized Euler Equations in Conservative Form
MODELING UNSTEADY FLOW EFFECTS IN A 3D TRANSONIC COMPRESSOR
Semi-implicit Preconditioning for Wall-bounded Flow
Jet Noise Modeling Using Synthetic Anisotropic Turbulence
Modeling of Synthetic Anisotropic Turbulence and its Sound Emission
A Study of Mach 0.75 Jets and Their Radiated Sound Using Large-Eddy Simulation
Aero Acoustic Investigation of an Open Cavity at Low Mach Number
Jet Noise Prediction Using Stochastic Turbulence Modeling
Large-Eddy Simulation of a Mach 0.75 Jet
TRANSFER OF UNSTEADY AND NON-AXISYMMETRIC EFFECTS IN THROUGHFLOW CALCULATIONS
Acoustic Source Terms for the Linear Euler Equations on Conservative Form
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Showing 1 research projects
Modal Decomposition of Separated Nozzle Flow