Static and Dynamic Simulations of the Pazy Wing Aeroelastic Benchmark by Nonlinear Potential Aerodynamics and detailed FE Model-Reference-Cited by-同舟云学术

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Static and Dynamic Simulations of the Pazy Wing Aeroelastic Benchmark by Nonlinear Potential Aerodynamics and detailed FE Model

Published:2021-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2021 Forum
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Author:

Ritter Markus¹,Hilger Jonathan¹,Zimmer Markus¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

1. Optimization, Manufacturing and Testing of a Composite Wing with Maximized Tip Deflection

2. Stiffness Optimization of Composite Wings with Aeroelastic Constraints

3. Dillinger, J., Static Aeroelastic Optimization of Composite Wings with Variable Stiffness Laminates, Ph.D. thesis,Delft University of Technology, June 2014.

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1. Accelerating aeroelastic UVLM simulations by inexact Newton algorithms;Computational Mechanics;2024-05-25

2. Collaborative Pazy Wing Analyses for the Third Aeroelastic Prediction Workshop;AIAA SCITECH 2024 Forum;2024-01-04

3. Aeroelastic Tailoring Framework of Pazy Wing With Variable Stiffness of Composites Spar;IEEE Access;2024

4. Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics;Journal of Aircraft;2023-09-25

5. Free wake panel method simulations of a highly flexible wing in flutter and gusts;Journal of Fluids and Structures;2023-08

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