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Precisely Controlled Two-Dimensional Rhombic Copolymer Micelles for Sensitive Flexible Tunneling Devices
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作者 Liang Han Hua Fan +5 位作者 Yulin Zhu Meijing Wang Feng Pan Dapeng Yu Yue Zhao Feng He 《CCS Chemistry》 CAS 2021年第5期1399-1409,共11页
Nanoscale two-dimensional(2D)organic materials have attracted significant interest on account of their unique properties,which result from their ultrathin and flat morphology.Supramolecular 2D nanomaterials prepared b... Nanoscale two-dimensional(2D)organic materials have attracted significant interest on account of their unique properties,which result from their ultrathin and flat morphology.Supramolecular 2D nanomaterials prepared by bottom-up approaches have great potential in the creation of nanoscale devices with various applications,each controlled by the properties of its single-molecular components.Here,we report a uniform and controllable 2D rhombic micelles formed by block copolymers(BCPs)with poly(p-phenylenevinylene)(PPV)as core blocks.The supramolecular 2D nanostructures created in this way and driven byπ-πinteractions realize the precise separation of the semiconducting and insulating constituents of the constructed BCPs.With a vertical tunneling device design,the 2D rhombic micelles exhibited an on-off current ratio of>10^(4)and a high on-state current density of 6000 A cm^(−2)as the insulating layer was compressed by a conductive atomic force microscopy(C-AFM)probe.The tunneling device also shows a reproducible sensitivity on a flexible substrate,opening up potential flexible pressure sensor applications for such novel supramolecular 2D nanostructures. 展开更多
关键词 block copolymer 2D self-assembly π-πinteraction controllable self-assembly tunneling device pressure sensor
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Shock Wave Strength Reduction by Passive Control Using Perforated Plates 被引量:2
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作者 Piotr Doerffer Oskar Szulc 《Journal of Thermal Science》 SCIE EI CAS CSCD 2007年第2期97-104,共8页
Strong, normal shock wave, terminating a local supersonic area on an airfoil, not only limits aerodynamic performance but also becomes a source of a high-speed impulsive helicopter noise. The application of a passive ... Strong, normal shock wave, terminating a local supersonic area on an airfoil, not only limits aerodynamic performance but also becomes a source of a high-speed impulsive helicopter noise. The application of a passive control system (a cavity covered by a perforated plate) on a rotor blade should reduce the noise created by a moving shock. This article covers the numerical implementation of the Bohning/Doerffer transpiration law into the SPARC code and includes an extended validation against the experimental data for relatively simple geometries of transonic nozzles. It is a first step towards a full simulation of a helicopter rotor equipped with a noise reducing passive control device in hover and in forward flight conditions. 展开更多
关键词 transonic flows shock wave - boundary layer interaction passive control.
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