Follow
Daniel Lindblad
Daniel Lindblad
Senior Research Scientist, CFD Software Entwicklungs- und Forschungsgesellschaft GmbH
Verified email at cfd-berlin.com
Title
Cited by
Cited by
Year
Implementation and run-time mesh refinement for the k− ω SST DES turbulence model when applied to airfoils
D Lindblad, A Jareteg, O Petit
Project work. Chalmers University of Technology, 2014
262014
Multi-objective optimization of an counter rotating open rotor using evolutionary algorithms
G Montero Villar, D Lindblad, N Andersson
2018 Multidisciplinary Analysis and Optimization Conference, 2929, 2018
172018
Effect of airfoil parametrization on the optimization of counter rotating open rotors
G Montero Villar, D Lindblad, N Andersson
AIAA Scitech 2019 Forum, 0698, 2019
102019
Aeroacoustic analysis of a counter rotating open rotor based on the harmonic balance method
D Lindblad, G Montero Villar, N Andersson, A Capitao Patrao, ...
2018 AIAA Aerospace Sciences Meeting, 1004, 2018
92018
Aerodynamic and aeroacoustic comparison of optimized high-speed propeller blades
A Capitao Patrao, D Lindblad, T Grönstedt
2018 Joint Propulsion Conference, 4658, 2018
72018
Implementation of a Quasi-Three-Dimensional Nonreflecting Blade Row Interface for Steady and Unsteady Analysis of Axial Turbomachines
D Lindblad, NA Wukie, G Montero Villar, N Andersson
2018 AIAA/CEAS Aeroacoustics Conference, 4187, 2018
72018
Minimizing aliasing in multiple frequency harmonic balance computations
D Lindblad, C Frey, L Junge, G Ashcroft, N Andersson
Journal of Scientific Computing 91 (2), 65, 2022
52022
Using horizontal sonic crystals to reduce the aeroacosutic signature of a simplified ICE3 train model
G Minelli, HD Yao, N Andersson, D Lindblad, J Forssén, P Höstmad, ...
Applied Acoustics 172, 107597, 2021
52021
A nonreflecting formulation for turbomachinery boundaries and blade row interfaces
D Lindblad, N Wukie, G Montero Villar, N Andersson
AIAA Scitech 2019 Forum, 1804, 2019
52019
Validating the Harmonic Balance Method for Turbomachinery Tonal Noise Predictions
D Lindblad, N Andersson
55th AIAA Aerospace Sciences Meeting, 2017
52017
Large Eddy Simulations of Isolated and Installed Jet Noise using the High-Order Discontinuous Galerkin Method
D Lindblad, SJ Sherwin, C Cantwell, J Lawrence, A Proenca, ...
AIAA SciTech 2023 Forum, 1546, 2023
42023
Aeroacoustic analysis of a subsonic jet using the discontinuous Galerkin method
D Lindblad, S Sherwin, C Cantwell, J Lawrence, A Proenca, ...
28th AIAA/CEAS Aeroacoustics 2022 Conference, 2932, 2022
42022
Investigation of Phase-Lagged Boundary Conditions for Turbulence Resolving Turbomachinery Simulations
G Montero Villar, D Lindblad, N Andersson
AIAA AVIATION 2020 FORUM, 2982, 2020
42020
Nonreflecting boundary conditions for the Euler equations in a discontinuous Galerkin discretization
NA Wukie, PD Orkwis, D Lindblad, N Andersson
AIAA Scitech 2019 Forum, 2172, 2019
32019
Convergence Acceleration of the Harmonic Balance Method Using a Time-Level Preconditioner
D Lindblad, N Andersson
AIAA Journal 58 (11), 4908-4922, 2020
22020
Aeroacoustic Analysis of a Closely Installed Chevron Nozzle Jet using the High-Order Discontinuous Galerkin Method
D Lindblad, SJ Sherwin, CD Cantwell, J Lawrence, A Proenca, ...
AIAA AVIATION 2023 Forum, 3831, 2023
12023
Numerical Methods for Aeroacoustic Analysis of Turbomachines
D Lindblad
PQDT-Global, 2020
12020
noisyduck: an open-source Python tool for computing eigenmode decompositions of duct flows
NA Wukie, D Lindblad, N Andersson
25th AIAA/CEAS Aeroacoustics Conference, 2418, 2019
12019
Nektar++: Development of the Compressible Flow Solver for Jet Aeroacoustics
D Lindblad, J Isler, MM Ginard, SJ Sherwin, CD Cantwell
Computer Physics Communications, 109203, 2024
2024
Nektar++: Development of the Compressible Flow Solver for Large Scale Aeroacoustic Applications
D Lindblad, J Isler, M Moragues, SJ Sherwin, C Cantwell
2023
The system can't perform the operation now. Try again later.
Articles 1–20