On a Bistable Flap for an Airfoil-Reference-Cited by-同舟云学术

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On a Bistable Flap for an Airfoil

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Daynes Stephen¹,Nall Sam¹,Weaver Paul¹,Potter Kevin¹,Margaris Panagiotis¹,Mellor Phil¹

Affiliation:

1. University of Bristol

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2103

Reference12 articles.

1. The Room-Temperature Shapes of Four-Layer Unsymmetric Cross-Ply Laminates

2. A concept for the generation of out-of-plane distortion from tailored FRP laminates

3. Bistable prestressed buckled laminates

4. Concepts for morphing airfoil sections using bi-stable laminated composite structures

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1. On maintaining bistability of prestressed laminates after clamping;Composite Structures;2024-09

2. On the Loss of Stability of Bistable Laminates due to Clamping;AIAA SCITECH 2024 Forum;2024-01-04

3. Thermally induced mechanical work and warpage compensation of asymmetric laminates;Composite Structures;2022-09

4. Study on snap-through actuation for the bistable composite laminated shell–MFC assembly;Mechanics of Advanced Materials and Structures;2022-02-04

5. Time-dependent shape of bistable unsymmetric carbon fibers-epoxy thin laminates;Smart Materials and Structures;2021-01-29

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