Add to ORKGIn the projects SmartLED and SADE a smart droop nose concept for a commercial transportation aircraft is developed by the partners EADS-IW, EADS-MAS and the DLR. The objective is a gap and step-less high lift device for the next generation aircraft of high surface quality for drag reduc-tion. The paper is focused on the preliminary experimental testing of a small section of a full-scale smart leading edge structure which is about to be tested in a ground test in the framework of the project SmartLED. The results of the experimental testing i.e. deformations of the structure and strains are compared to predictions from FE analyses of droop angles of 5°,10° and 16°
A smoothly varying extreme-displacement morphing droop-nose as a novel high-lift device has the pote...
At the Institute of Composite Structures and Adaptive systems (FA, Prof. Wiedemann) of the DLR the s...
At the Institute of Composite Structures and Adaptive Systems (FA, Prof. Wiedemann) of the DLR the s...
In the projects SmartLED and SADE a smart droop nose concept for a commercial transportation aircraf...
Within the framework of the fourth national German research program for aeronautics a fiber rein-for...
A seamless and gapless high lift device at the wing’s leading edge has the potential for reduction o...
A seamless and gapless high lift device at the wing’s leading edge has the potential for reduction o...
Since 2007 the DLR Institute of Composite Structures and Adaptive Systems investigates the smart Dro...
The presented paper describes the pre-design and sizing of a smart leading edge section which is dev...
The presented paper describes the pre-design and sizing of a smart leading edge section which is dev...
The manufacture and ground testing of a 3D full-scale 1100 mm span morphing wing leading edge device...
The high lift systems of modern-day commercial airplanes are highly effective systems providing the ...
To make use of low-drag future generation wings with high aspect ratio and low sweep for natural lam...
For the application of laminar flow on commercial aircraft wings the high-lift devices at the leadin...
Because of the large potential of drag reduction natural laminar flow is one of the challenging aims...
A smoothly varying extreme-displacement morphing droop-nose as a novel high-lift device has the pote...
At the Institute of Composite Structures and Adaptive systems (FA, Prof. Wiedemann) of the DLR the s...
At the Institute of Composite Structures and Adaptive Systems (FA, Prof. Wiedemann) of the DLR the s...
In the projects SmartLED and SADE a smart droop nose concept for a commercial transportation aircraf...
Within the framework of the fourth national German research program for aeronautics a fiber rein-for...
A seamless and gapless high lift device at the wing’s leading edge has the potential for reduction o...
A seamless and gapless high lift device at the wing’s leading edge has the potential for reduction o...
Since 2007 the DLR Institute of Composite Structures and Adaptive Systems investigates the smart Dro...
The presented paper describes the pre-design and sizing of a smart leading edge section which is dev...
The presented paper describes the pre-design and sizing of a smart leading edge section which is dev...
The manufacture and ground testing of a 3D full-scale 1100 mm span morphing wing leading edge device...
The high lift systems of modern-day commercial airplanes are highly effective systems providing the ...
To make use of low-drag future generation wings with high aspect ratio and low sweep for natural lam...
For the application of laminar flow on commercial aircraft wings the high-lift devices at the leadin...
Because of the large potential of drag reduction natural laminar flow is one of the challenging aims...
A smoothly varying extreme-displacement morphing droop-nose as a novel high-lift device has the pote...
At the Institute of Composite Structures and Adaptive systems (FA, Prof. Wiedemann) of the DLR the s...
At the Institute of Composite Structures and Adaptive Systems (FA, Prof. Wiedemann) of the DLR the s...