21–29 von 29 Ergebnissen
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    Estimating Flutter Bifurcation Diagrams Using the State Velocity

    Riso, Cristina / Cesnik, Carlos E. S. / Epureanu, Bogdan I. | AIAA | 2022

    This paper introduces a method for estimating flutter bifurcation diagrams of systems described by time-domain state-space models. The

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Wings

    Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction

    He, Sicheng / Jonsson, Eirikur / Mader, Charles A. et al. | AIAA | 2021

    Flutter and limit cycle oscillation (LCO) are important phenomena that need to be considered in aircraft design. Previous harmonic

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Design

    Physics-Based Data-Driven Buffet-Onset Constraint for Aerodynamic Shape Optimization

    Li, Jichao / He, Sicheng / Zhang, Mengqi et al. | AIAA | 2022
    is still a lack of accurate and efficient buffet formulation to impose the constraint. This work proposes a physics-based data-driven buffet ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Design

    Toward Automatic Parabolized Stability Equation-Based Transition-to-Turbulence Prediction for Aerodynamic Flows

    Olichevis Halila, Gustavo Luiz / Fidkowski, Krzysztof J. / Martins, Joaquim R. R. A. | AIAA | 2020

    The inclusion of transition-to-turbulence effects in computational fluid dynamics simulations is essential to accurately predict drag

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Configurations

    Component-Based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes

    Secco, Ney R. / Jasa, John P. / Kenway, Gaetan K. W. et al. | AIAA | 2018
    aircraft components overlap to model the full aircraft configuration. However, from the standpoint of geometry manipulation, most methods operate ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Configurations

    Sensitivity-Based Geometric Parametrization and Automatic Scaling for Aerodynamic Shape Optimization

    Wu, Neil / Mader, Charles A. / Martins, Joaquim R. R. A. | AIAA | 2023

    Aerodynamic shape optimization has become well established, with designers routinely performing wing and full aircraft optimizations

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    Verlag: The American Institute of Aeronautics and Astronautics

    Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization

    Kenway, Gaetan K. W. / Martins, Joaquim R. R. A. | AIAA | 2017

    High-fidelity computational modeling and optimization of aircraft configurations have the potential to enable engineers to create more

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Configurations

    Linear Stability-Based Smooth Reynolds-Averaged Navier–Stokes Transition Model for Aerodynamic Flows

    Halila, Gustavo Luiz Olichevis / Yildirim, Anil / Mader, Charles A. et al. | AIAA | 2021
    in parts of the aircraft in multiple flight conditions. Modified Reynolds-averaged Navier–Stokes (RANS) models that consider transition ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization

    Secco, Ney R. / Kenway, Gaetan K. W. / He, Ping et al. | AIAA | 2021
    deformed meshes may contain bad-quality cells that degrade the accuracy of computational fluid dynamics (CFD) solvers. Moreover, an inefficient ...
    Verlag: The American Institute of Aeronautics and Astronautics