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Aircraft
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title: Smart Intelligent Aircraft Structures (SARISTU)
Manufacturing and Testing of Smart Morphing SARISTU Trailing Edge
Assessment of the SARISTU Enhanced Adaptive Droop Nose
For the application of laminar flow on commercial aircraft wings, the high-lift devices at the leading edge play
...SARISTU: Six Years of Project Management
SARISTU—Smart Intelligent Aircraft Structures—is a large, integrated research and technology project funded by
...Benefit Analysis Value and Risk Assessment of New SARISTU-Technologies
The value and risk assessment investigates whether the SARISTU aim of improving aircraft efficiency has been met
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Within the SARISTU project, the Application Scenario 5 (AS05) was devoted primarily to the development of
...Morphing Value Assessment on Overall Aircraft Level
In order to assess the benefit of the morphing devices developed in the framework of SARISTU, integration in an
...Manufacturing of Nano-treated Lower Panel Demonstrators for Aircraft Fuselage
Shape Sensing for Morphing Structures Using Fiber Bragg Grating Technology
Damage Assessment in Composite Structures Based on Acousto-Ultrasonics—Evaluation of Performance
Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysis
Improvement of the Electrical Isotropy of Composite Structures—Overview
The aim of SARISTU is to take forward to higher TRL level from previous research various technologies and methods
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Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge
Within the scope of the SARISTU project (smart intelligent aircraft structures), a wingtip active trailing edge
...Load Monitoring by Means of Optical Fibres and Strain Gages
This chapter describes the development of load monitoring systems integrated in the demonstrator of a smart wing
...Development of a Door Surround Structure with Integrated Structural Health Monitoring System
Winglet Design, Manufacturing, and Testing
With respect to the SARISTU project (Smart Intelligent Aircraft Structures), a wingtip active trailing edge (WATE
...Development and Validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose
In the frame of IS12 wing integration scenario of the SARISTU project, SONACA was incharge of the development and
...Use of Carbon Nanotubes in Structural Composites
Ribbon Tapes, Shape Sensors, and Hardware
For fiber optic sensors to be integrated in aerospace structures and for these sensors to provide data that can
...Path-Based MAPOD Using Numerical Simulations
Morphing Wing Integrated Safety Approach and Results
SARISTU morphing wing is mainly based on three devices: enhanced adaptive droop nose (EADN), adaptive trailing
...Damage Introduction, Detection, and Assessment at CFRP Door Surrounding Panel
Coating for Detecting Damage with a Manifest Color Change
Carbon fiber-reinforced plastic (CFRP) structures are used in modern airliner. An impact may damage the inner
...Implementation of a Structural Health Monitoring System for a Composite Wing Box Skin
Flat and Curved Panel Manufacturing
Metallic Strip Details for Validation of ESN Technologies
The aim of AS10 is to evaluate technologies that can be integrated directly into structures with the target of
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The extended use of CFRP material in airframes led to a loss of the ability to use the aircraft superstructure
...Testing Overview of the EADN Samples
Enhancement of Primary Structure Robustness by Improved Damage Tolerance
The aim of SARISTU is to take forward to higher TRL level from previous research of various technologies and
...Enhanced Adaptive Droop Nose—from Computer Model to Multi-functional Integrated Part
The INVENT GmbH rises in the EU project SARISTU under the lead of Airbus and in cooperation with project partners
...Fabrication of Carbon Nanotubes-Doped Veils
Damage tolerance of aircraft primary structures is important to prolong the life of the structure and reduce
...Sensitive Coating Solutions to Lower BVID Threshold on Composite Structure
The objectives of the 8th Application Scenario in SARISTU project is to develop sensitive coating for impact
...Piezochromic Compounds Able to be Used in Shock Detecting Paints
Design and manufacturing of a curved stiffened panel has been carried out within WP135 in SARISTU Integration
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Toward the Upscaling of Guided Waves-Based NDE and SHM in Aeronautics
PAMELA SHM System Implementation on Composite Wing Panels