Design of Shape-Adaptive Deployable Slat-Cove Filler for Airframe Noise Reduction-Reference-Cited by-同舟云学术

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Design of Shape-Adaptive Deployable Slat-Cove Filler for Airframe Noise Reduction

Published:2021-09 Issue:5 Volume:58 Page:1034-1050
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Arena Gaetano,Groh Rainer M. J.,Pirrera Alberto,Turner Travis¹,Scholten William,Hartl Darren

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Funder

Langley Research Center

Royal Academy of Engineering

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036070

Reference44 articles.

1. Initial Thoughts on Weight Penalty Effects in Shape-adaptable Systems

2. Aerodynamic Performance of the Smart Wing Control Effectors

3. Morphing Aircraft Systems: Historical Perspectives and Future Challenges

4. ADAPTIVE-PASSIVE ABSORBERS USING SHAPE-MEMORY ALLOYS

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1. Aeroelasticity Model for Highly Flexible Aircraft Based on the Vortex Lattice Method;Aerospace;2023-09-14

2. Effects of bulb seal on slat flow dynamics and slat tones;European Journal of Mechanics - B/Fluids;2023-07

3. Structural function from sequential, interacting elastic instabilities;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2023-04

4. Structural morphing induced by functionalising buckling;Thin-Walled Structures;2022-12

5. Functionalising buckling for structural morphing in kinetic façades: Concepts, strategies and applications;Thin-Walled Structures;2022-11

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