Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests-Reference-Cited by-同舟云学术

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Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests

Published:2017-03 Issue:2 Volume:54 Page:519-534
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Vasista Srinivas,Riemenschneider Johannes,van de Kamp Bram,Monner Hans Peter,Cheung Ronald C. M.,Wales Christopher,Cooper Jonathan E.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033909

Reference36 articles.

1. Design of a smart leading edge device for low speed wind tunnel tests in the European project SADE

2. Design and Analysis of a Droop Nose for Coanda Flap Applications

3. Experimental Evaluation of the Morphing Leading Edge Concept

4. Design of Compliant Mechanisms for Morphing Structural Shapes

5. An Effective Method of Synthesizing Compliant Adaptive Structures using Load Path Representation

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1. Improvement in the Ice Tolerance of a Swept Wing Based on the Drooping Leading Edge;2024

2. Honeycomb structure filling morphing wing trailing edge: Design strategy, deformation feedback, and active control;Programmable Materials;2024

3. Large Deflection Model and Optimal Design for a Morphing Wing Leading-Edge Skin;Journal of Aircraft;2023-11-21

4. Anisotropic flexure hinges: Manufacturing and mechanical characterization for application in pressure-actuated morphing structures;Composites Part B: Engineering;2023-11

5. Final validation and performance assessment of a full-scale morphing droop nose demonstrator;AIAA SCITECH 2023 Forum;2023-01-19

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