Sloshing reduced-order models for aeroelastic analyses of innovative aircraft configurations-Reference-Cited by-同舟云学术

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Sloshing reduced-order models for aeroelastic analyses of innovative aircraft configurations

Published:2021-11 Issue: Volume:118 Page:107075
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Colella Marta^ORCID,Saltari Francesco,Pizzoli Marco,Mastroddi Franco^ORCID

Funder

H2020

Horizon 2020

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. Finite-element based modeling for flight dynamics and aeroelasticity of flexible aircraft;Saltari;J. Aircr.,2017

2. The Dynamic Behavior of Liquids in Moving Containers with Applications to Space Vehicle Technology;Abramson,1966

3. Liquid Sloshing Dynamics: Theory and Applications;Ibrahim,2005

4. The Characteristics of Fuel Motion which Affect Airplane Dynamics;Graham,1951

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1. Adaptive dynamic programming base on MMC device of a flexible high-altitude long endurance aircraft;Aerospace Science and Technology;2024-08

2. Flight test of flying wing aircraft controlled by dual synthetic jets at Ma0.2;Aerospace Science and Technology;2024-01

3. Sloshing reduced-order model trained with Smoothed Particle Hydrodynamics simulations;Nonlinear Dynamics;2023-10-03

4. Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling;Journal of Aircraft;2023-09-03

5. A data-driven reduced-order model for rotor optimization;Wind Energy Science;2023-07-20

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