Manufacture and Testing of a Large-displacement Droop-Nose Morphing Wing Leading Edge
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. Technical University of Braunschweig
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1858
Reference11 articles.
1. SFB 880: fundamentals of high lift for future commercial aircraft
2. Design and Analysis of a Droop Nose for Coanda Flap Applications
3. Design of a smart leading edge device for low speed wind tunnel tests in the European project SADE
4. Experimental Evaluation of the Morphing Leading Edge Concept
5. Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests
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2. Low Speed Wind Tunnel Test Method and Structural Function Verification of Variable Camber Wing Leading Edge Full Scale Prototype;Lecture Notes in Electrical Engineering;2024
3. A Review on Fishbone Active Camber Morphing Wing Surfaces;New Technologies and Developments in Unmanned Systems;2023
4. Large-Displacement Morphing Wing Leading Edge Droop Nose: Optimization, Manufacture and Instrumentation;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-18
5. Development of a hybrid (rigid-flexible) morphing leading edge equipped with bending and extending capabilities;Journal of Intelligent Material Systems and Structures;2020-09-12
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