國立高雄大學圖資館 |

語系: 繁體中文

說明(常見問題)

圖資館首頁

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Smart Intelligent Aircraft Structure...

Papadopoulos, Michael.

Smart Intelligent Aircraft Structures (SARISTU)proceedings of the Final Project Conference /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Smart Intelligent Aircraft Structures (SARISTU)edited by Piet Christof Wolcken, Michael Papadopoulos.
其他題名:	proceedings of the Final Project Conference /
其他作者:	Wolcken, Piet Christof.
出版者:	Cham :Springer International Publishing :2016.
面頁冊數:	xxviii, 1039 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer eBooks
標題:	AirplanesCongresses.Technological innovations
電子資源:	http://dx.doi.org/10.1007/978-3-319-22413-8
ISBN:	9783319224138$q(electronic bk.)

Smart Intelligent Aircraft Structures (SARISTU)proceedings of the Final Project Conference /
Smart Intelligent Aircraft Structures (SARISTU)proceedings of the Final Project Conference /[electronic resource] :edited by Piet Christof Wolcken, Michael Papadopoulos. - Cham :Springer International Publishing :2016. - xxviii, 1039 p. :ill. (some col.), digital ;24 cm.

SARISTU: Six years of project management -- Morphing Wing integrated safety approach and results -- Development and validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose -- Adaptive Trailing Edge: Specifications, Aerodynamics and Exploitation -- Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanes -- Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge -- Winglet design, manufacturing and testing -- Ribbon tapes, shape sensors and hardware -- Methodologies for the Damage Detection based on Fiber Optic sensors. Applications to the fuselage panel and lower wing panel -- Methodologies for guided waves based SHM system implementation on composite wing panels: results and perspectives from SARISTU Scenario 5 -- An electro-mechanical impedance based mobile system for structural health monitoring and reliability check of bonded piezoelectric sensors -- Damage Identification in Composite Panels - Methodologies and Visualisation -- Manufacturing of CFRP panels with integrated sensor network and contacting of the network -- Flat and curved panel manufacturing -- Compression after multiple impacts: modelling and experimental validation on composite coupon specimens -- Piezochromic compounds able to be used in shock detecting paints -- Brittle coating layers for impact detection in CFRP -- Use of Carbon Nanotubes in Structural Composites -- Enhancement of primary structure robustness by improved damage tolerance -- Improvement of the electrical isotropy of composite structures- Overview -- Fabrication of carbon nanotubes doped veils -- Morphing value assessment on overall aircraft level -- Implementation of Morphing, Structural Health Monitoring and Nanomaterials on an Outer Wing Box -- Fuselage Demonstrators: An overview of the development approach -- Development of a Door Surround Structure with Integrated Structural Health Monitoring System.

The book includes the research papers presented in the final conference of the EU funded SARISTU (Smart Intelligent Aircraft Structures) project, held at Moscow, Russia between 19-21 of May 2015. The SARISTU project, which was launched in September 2011, developed and tested a variety of individual applications as well as their combinations. With a strong focus on actual physical integration and subsequent material and structural testing, SARISTU has been responsible for important progress on the route to industrialization of structure integrated functionalities such as Conformal Morphing, Structural Health Monitoring and Nanocomposites. The gap- and edge-free deformation of aerodynamic surfaces known as conformal morphing has gained previously unrealized capabilities such as inherent de-icing, erosion protection and lightning strike protection, while at the same time the technological risk has been greatly reduced. Individual structural health monitoring techniques can now be applied at the part-manufacturing level rather than via extending an aircraft's time in the final assembly line. And nanocomposites no longer lose their improved properties when trying to upscale from neat resin testing to full laminate testing at element level. As such, this book familiarizes the reader with the most significant develo pments, achievements and key technological steps which have been made possible through the four-year long cooperation of 64 leading entities from 16 different countries with the financial support of the European Commission.

ISBN: 9783319224138$q(electronic bk.)

Standard No.: 10.1007/978-3-319-22413-8doiSubjects--Topical Terms:

737724
Airplanes
--Technological innovations--Congresses.

LC Class. No.: TL671.2

Dewey Class. No.: 629.1341

Smart Intelligent Aircraft Structures (SARISTU)proceedings of the Final Project Conference /
LDR:04553nmm a2200325 a 4500 001 481575
003 DE-He213
005 20160721092106.0
006 m d
007 cr nn 008maaau
008 161007s2016 gw s 0 eng d
020 $a 9783319224138$q(electronic bk.)
020 $a 9783319224121$q(paper)
024 7 $a 10.1007/978-3-319-22413-8 $2 doi
035 $a 978-3-319-22413-8
040 $a GP $c GP
041 0 $a eng
050 4 $a TL671.2
072 7 $a TRP $2 bicssc
072 7 $a TTDS $2 bicssc
072 7 $a TEC002000 $2 bisacsh
082 0 4 $a 629.1341 $2 23
090 $a TL671.2 $b .S636 2016
245 0 0 $a Smart Intelligent Aircraft Structures (SARISTU) $h [electronic resource] : $b proceedings of the Final Project Conference / $c edited by Piet Christof Wolcken, Michael Papadopoulos.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2016.
300 $a xxviii, 1039 p. : $b ill. (some col.), digital ; $c 24 cm.
505 0 $a SARISTU: Six years of project management -- Morphing Wing integrated safety approach and results -- Development and validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose -- Adaptive Trailing Edge: Specifications, Aerodynamics and Exploitation -- Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanes -- Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge -- Winglet design, manufacturing and testing -- Ribbon tapes, shape sensors and hardware -- Methodologies for the Damage Detection based on Fiber Optic sensors. Applications to the fuselage panel and lower wing panel -- Methodologies for guided waves based SHM system implementation on composite wing panels: results and perspectives from SARISTU Scenario 5 -- An electro-mechanical impedance based mobile system for structural health monitoring and reliability check of bonded piezoelectric sensors -- Damage Identification in Composite Panels - Methodologies and Visualisation -- Manufacturing of CFRP panels with integrated sensor network and contacting of the network -- Flat and curved panel manufacturing -- Compression after multiple impacts: modelling and experimental validation on composite coupon specimens -- Piezochromic compounds able to be used in shock detecting paints -- Brittle coating layers for impact detection in CFRP -- Use of Carbon Nanotubes in Structural Composites -- Enhancement of primary structure robustness by improved damage tolerance -- Improvement of the electrical isotropy of composite structures- Overview -- Fabrication of carbon nanotubes doped veils -- Morphing value assessment on overall aircraft level -- Implementation of Morphing, Structural Health Monitoring and Nanomaterials on an Outer Wing Box -- Fuselage Demonstrators: An overview of the development approach -- Development of a Door Surround Structure with Integrated Structural Health Monitoring System.
520 $a The book includes the research papers presented in the final conference of the EU funded SARISTU (Smart Intelligent Aircraft Structures) project, held at Moscow, Russia between 19-21 of May 2015. The SARISTU project, which was launched in September 2011, developed and tested a variety of individual applications as well as their combinations. With a strong focus on actual physical integration and subsequent material and structural testing, SARISTU has been responsible for important progress on the route to industrialization of structure integrated functionalities such as Conformal Morphing, Structural Health Monitoring and Nanocomposites. The gap- and edge-free deformation of aerodynamic surfaces known as conformal morphing has gained previously unrealized capabilities such as inherent de-icing, erosion protection and lightning strike protection, while at the same time the technological risk has been greatly reduced. Individual structural health monitoring techniques can now be applied at the part-manufacturing level rather than via extending an aircraft's time in the final assembly line. And nanocomposites no longer lose their improved properties when trying to upscale from neat resin testing to full laminate testing at element level. As such, this book familiarizes the reader with the most significant develo pments, achievements and key technological steps which have been made possible through the four-year long cooperation of 64 leading entities from 16 different countries with the financial support of the European Commission.
650 0 $a Airplanes $x Technological innovations $v Congresses. $3 737724
650 0 $a Airplanes $x Design and construction $v Congresses. $3 384664
650 0 $a Airplanes $x Electronic equipment $v Congresses. $3 737725
650 0 $a Aeronautics $v Human factors. $3 452229
650 1 4 $a Engineering. $3 210888
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
650 2 4 $a Materials Engineering. $3 682881
650 2 4 $a Nanotechnology. $3 193873
700 1 $a Wolcken, Piet Christof. $3 737722
700 1 $a Papadopoulos, Michael. $3 737723
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer eBooks
856 4 0 $u http://dx.doi.org/10.1007/978-3-319-22413-8
950 $a Engineering (Springer-11647)