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_aSpringerLink (Online service) _9106996 |
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_c119237 _d119237 |
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| 001 | 119237 | ||
| 003 | ES-MaUEC | ||
| 005 | 20230102113936.0 | ||
| 006 | a||||fo|||| 00| 0 | ||
| 007 | cr nn nnnaamaa | ||
| 008 | 200313s2020 gw | s |||| 0|eng d | ||
| 020 | _a9783030365141 | ||
| 024 | 7 |
_a10.1007/978-3-030-36514-1 _2doi |
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| 040 |
_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC |
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| 050 | 4 |
_aTL545 _b2020 EB |
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| 245 | 1 | 0 |
_aFlexible Engineering Toward Green Aircraft. _bCAE Tools for Sustainable Mobility _cedited by Marco Evangelos Biancolini, Ubaldo Cella |
| 250 | _aFirst edition 2020. | ||
| 264 | 1 |
_aCham _bSpringer International Publishing _c2020 |
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| 300 |
_a1 recurso en línea (XII, 187 páginas) _b130 ilustraciones, 77 ilustraciones a color |
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| 336 |
_2rdacontent _aTexto _btxt |
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| 337 |
_2rdamedia _aelectrónico _bc |
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| 338 |
_2rdacarrier _arecurso electrónico _bcr |
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| 347 |
_aArchivo de texto _bPDF |
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| 490 | 0 |
_aLecture Notes in Applied and Computational Mechanics _x1613-7736 _v92 |
|
| 490 | 0 | _aEngineering (Springer-11647) | |
| 505 | 0 | _aThe next generation of aircraft -- Aeroelastic wind tunnel tests of the RIBES wing model -- Validation of high fidelity computational methods for aeronautical FSI analyses -- High-fidelity static aeroelastic simulations of the Common Research Model -- Aero-elastic simulations using the NSMB CFD solver including results for a Strut Braced Wing -- Semi-analytical modeling of non-stationary fluid-structure interaction -- Fluid structure modelling of ground induced vibrations by mesh morphing and modal superposition -- Unsteady FSI Analysis of a Square Array of Tubes in Water Crossflow -- Risk measures applied to robust aerodynamic shape design optimization -- Aero-structural Optimization of a MALE configuration in the AGILE MDO Framework. | |
| 520 | 3 | _aThis book discusses the recent advances in aircraft design methodologies. It provides an overview of topics such as shape optimization, robust design and aeroelasticity, focusing on fluid-structure numerical methodologies to address static and dynamic aeroelastic problems. It demonstrates that the capability to evaluate the interaction between aerodynamics, inertia and elastic forces is important to avoid drag penalties, control system efficiency loss and generation of potentially dangerous phenomena, such as divergence, control reversal and flutter. The book particularly highlights the advances in "high fidelity" CFD-CSM coupling, describing the latest experimental research to validate the numerical fluid-structure interaction analysis methodologies resulting from the EU-funded RBF4AERO and RIBES projects. | |
| 988 | _aSpringer_Engineering_31032020 | ||
| 650 | 7 |
_2embne _aAeronáutica _9667366 |
|
| 700 | 1 |
_aBiancolini, Marco Evangelos _eeditor _4edt _4http://id.loc.gov/vocabulary/relators/edt |
|
| 700 | 1 |
_aCella, Ubaldo _eeditor _4edt _4http://id.loc.gov/vocabulary/relators/edt |
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| 773 | 0 | _tSpringer eBooks | |
| 776 | 0 | 8 |
_iPrinted edition: _z9783030365134 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783030365158 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783030365165 |
| 856 | 4 | 0 |
_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-36514-1 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid) |
| 942 |
_2lcc _cLE |
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| 998 |
_b04/2020 _dz _ek _zSI |
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