Elastic Axis Determination and Extraction of Vibration Mode Shapes of a Light Weight Composite Aircraft-Reference-Cited by-同舟云学术

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Elastic Axis Determination and Extraction of Vibration Mode Shapes of a Light Weight Composite Aircraft

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 Multidisciplinary Analysis and Optimization Conference
language:
Short-container-title:

Author:

Jrad Mohamed¹,Zhao Wei¹,Kapania Rakesh K.¹,Schmidt David²

Affiliation:

1. Virginia Polytechnic Institute and State University

2. D K Schmidt & Associates

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3429

Reference19 articles.

1. Flight-Dynamics and Flutter Modeling and Analyses of a Flexible Flying-Wing Drone - Invited

2. Determination of Elastic Wing Aerodynamic Characteristics

3. Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered plates

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1. Nonlinear Low-Fidelity Numerical Model of the Flared Folding Wingtip;AIAA SCITECH 2023 Forum;2023-01-19

2. Aeroelastic Modeling of UAM Conceptual Vehicles;AIAA SCITECH 2022 Forum;2022-01-03

3. mAEWing2: Initial Flight Test and System Identification of a Flexible UAV;AIAA Scitech 2020 Forum;2020-01-05

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