Institution
Airbus
Company•Bengaluru, Karnataka, India•
About: Airbus is a company organization based out in Bengaluru, Karnataka, India. It is known for research contribution in the topics: Fuselage & Signal. The organization has 10633 authors who have published 13089 publications receiving 88354 citations. The organization is also known as: Airbus Commercial Aircraft.
Topics: Fuselage, Signal, Wing, Layer (electronics), Rotor (electric)
Papers published on a yearly basis
Papers
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12 Jun 2000TL;DR: In this article, a comfort and illumination unit for a passenger space in an aircraft is constructed for cooperation with a straight wall panel that can be integrated in or secured to a vertical straight wall and/or a horizontal straight ceiling wall.
Abstract: A comfort and illumination unit especially for a passenger space in an aircraft is constructed for cooperation with a straight wall panel that can be integrated in or secured to a vertical straight wall and/or a horizontal straight ceiling wall. The unit has a mounting base and a cover with passenger convenience elements mounted to the base under the cover which is provided with cut-outs for access to the convenience elements. Fluorescent bulbs form a frame around the convenience elements.
24 citations
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TL;DR: In this article, the behavior of a composite reinforced cylinder under various loadings is analyzed and an optimization procedure is presented to choose the most efficient values of the geometric parameters defining the composite reinforcements and the position of the stiffeners on the surface of the cylinder.
24 citations
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07 Jun 2010TL;DR: Acoustic and resistance measurements were performed in NLR's Small Anechoic Wind Tunnel on a large number of meshes intended for landing gear noise reduction, finding that the meshes yield a drastic broadband noise reduction for a wide range of mesh materials and mesh shapes.
Abstract: Acoustic and resistance measurements were performed in NLR's Small Anechoic Wind Tunnel on a large number of meshes intended for landing gear noise reduction. The meshes were tested on generic bluff bodies which simulated single and combined landing gear struts. An out-of-flow microphone array was used to localize and quantify the noise sources on the model. It is found that the meshes yield a drastic broadband noise reduction for a wide range of mesh materials and mesh shapes. The noise reduction occurs for all tested angles of attack and for all tested models. For the combined bodies it is found to be sufficient to treat only the upstream component with a mesh.
24 citations
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23 Mar 2010TL;DR: In this article, a method of joining a first component to a second component is proposed, which consists of forming an array of projections extending from a bond surface of the first component, the projections having a plurality of different profiles.
Abstract: A method of joining a first component to a second component, the method comprising forming an array of projections extending from a bond surface of the first component, the projections having a plurality of different profiles; and embedding the array of projections in the second component formed of a plurality of laminate plies, wherein each projection profile is adapted to best transfer load into a respective one of the laminate plies. The resultant joint is able to transfer load more progressively between the two components leading to improved tensile strength.
24 citations
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TL;DR: In this article, a hybrid thermal protection system for aerospace applications based on ablative material (ASTERM) and ceramic matrix composite (SICARBON) was investigated using graphite and zirconia-zirconium silicate based commercial high temperature adhesives.
Abstract: Hybrid thermal protection systems for aerospace applications based on ablative material (ASTERM™) and ceramic matrix composite (SICARBON™) have been investigated. The ablative material and the ceramic matrix composite were joined using graphite and zirconia–zirconium silicate based commercial high temperature adhesives. The thermo-mechanical performance of the structures was assessed from room temperature up to 900 °C. In all the joints there is a decrease of shear strength with the increase of temperature. Analysis of the fractured surfaces showed that above 150 °C the predominant mode of fracture is cohesive failure in the bonding layer. The joints fabricated with the zirconia–zirconium silicate based adhesive present the best performance and they have the potential to be used as hybrid thermal protection systems for aerospace applications in the temperature range 700–900 °C.
24 citations
Authors
Showing all 10636 results
Name | H-index | Papers | Citations |
---|---|---|---|
Xin Zhang | 87 | 1714 | 40102 |
Hui Ying Yang | 67 | 393 | 15269 |
Richard J. Wong | 64 | 282 | 13922 |
Gerhard Müller | 52 | 453 | 11096 |
Mayank Jain | 50 | 271 | 12429 |
Olivier de Weck | 41 | 351 | 7948 |
Kay Hameyer | 41 | 753 | 7275 |
Raed Mesleh | 40 | 185 | 10244 |
Scott R. Presnell | 39 | 178 | 10095 |
Thuc P. Vo | 38 | 108 | 4450 |
Ashutosh Tiwari | 37 | 249 | 7258 |
Ulrich Schmid | 36 | 617 | 5897 |
Elmar Bonaccurso | 36 | 115 | 4729 |
Kaiming Zhou | 36 | 238 | 3979 |
Norman M. Ratcliffe | 35 | 105 | 4895 |