Overview and summary of the second AIAA high-lift prediction workshop
CL Rumsey, JP Slotnick - Journal of Aircraft, 2015 - arc.aiaa.org
The Second AIAA CFD High-Lift Prediction Workshop was held in San Diego, California in
June 2013. The goals of the workshop continued in the tradition of the first high-lift …
June 2013. The goals of the workshop continued in the tradition of the first high-lift …
Rans solutions on high lift common research model with scFLOW, a polyhedral finite-volume solver
Y Nakashima, Y Ando, S Taguchi, T Itami… - AIAA Aviation 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3522. vid Reynolds-averaged
Navier-Stokes (RANS) solutions obtained with scFLOW, a polyhedral finite-volume solver …
Navier-Stokes (RANS) solutions obtained with scFLOW, a polyhedral finite-volume solver …
Lattice-Boltzmann simulations of an oscillating NACA0012 airfoil in dynamic stall
Unsteady two and three-dimensional flow simulations of an oscillating airfoil are performed
using the Lattice-Boltzmann CFD approach. A sliding mesh is employed, in order to …
using the Lattice-Boltzmann CFD approach. A sliding mesh is employed, in order to …
Static hysteresis of the aerodynamic characteristics of a model aircraft in the landing regime
AV Voevodin, VG Soudakov - Fluid Dynamics, 2018 - Springer
Flow past a simplified model of the civil aircraft is numerically investigated in the landing
regime. The numerical modeling is performed within the framework of the Reynolds …
regime. The numerical modeling is performed within the framework of the Reynolds …
Validation of a Low Dissipation Lattice-Boltzmann Method for Transonic Flows in Aerospace Applications
RF Vieira, S Noelting, S Muthu… - … FORUM AND ASCEND …, 2024 - arc.aiaa.org
An extended Lattice-Boltzmann Method (LBM) for the simulation of transonic flows is
proposed for increasing the Mach number range of the regular method while preserving its …
proposed for increasing the Mach number range of the regular method while preserving its …
Lattice Boltzmann Simulation of a Deploying Krueger Flap Device
J Ponsin, C Lozano - Advanced Computational Methods and Design for …, 2024 - Springer
We describe the performance of a lattice Boltzmann method for predicting the flow features
of the turbulent unsteady flow generated during the motion of a Krueger flap designed for …
of the turbulent unsteady flow generated during the motion of a Krueger flap designed for …
Статический гистерезис аэродинамических характеристик модели самолета на посадочном режиме
ВГ Судаков, АВ Воеводин - … академии наук. Механика жидкости и газа, 2018 - elibrary.ru
Представлены результаты расчетных исследований обтекания упрощенной модели
компоновки гражданского самолета на посадочном режиме. Численное моделирование …
компоновки гражданского самолета на посадочном режиме. Численное моделирование …
[PDF][PDF] Untersuchung der Strömungsstruktur um einen Deltaflügel mit scharfer Vorderkante bei unterschiedlichen Vorderkantenpfeilungen mit einem Lattice-Boltzmann …
A Muhr, E Özger - 2015 - dglr.de
Zusammenfassung" DWLBM-Investigation of Delta Wing Time Dependent Flow
Characteristics with Lattice-Boltzmann Method" ist ein Forschungsprojekt der Fakultät für …
Characteristics with Lattice-Boltzmann Method" ist ein Forschungsprojekt der Fakultät für …