Multi-Material Printed Trailing Edge Control Surface for an Aeroservoelastic Wind Tunnel Model-Reference-Cited by-同舟云学术

Multi-Material Printed Trailing Edge Control Surface for an Aeroservoelastic Wind Tunnel Model

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

Author:

Pankonien Alexander M.¹,Durscher Ryan¹,Bhagat Nitin D.²,Reich Gregory¹

Affiliation:

1. Air Force Research Laboratory

2. University of Dayton Research Institute

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2930

Reference12 articles.

1. "Chapter 6: Innovating Clean Energy Technologies in Advanced Manufacturing, Technology Assessments, 6A, Additive Manufacturing,' Department of Energy Quadrennial Technology Review, 2015.

2. 3D-Printed Wind Tunnel Flutter Model

3. Optimal Structural Topology of a Platelike Wing for Subsonic Aeroelastic Stability

4. Level Set Topology Optimisation of Aircraft Wing Considering Aerostructural Interaction

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