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| 001 | 79502 | ||
| 003 | ES-MaUEC | ||
| 005 | 20230307040205.0 | ||
| 008 | 160527s2014 uik b 001 0 eng d | ||
| 020 | _a9780470662571 | ||
| 040 |
_aDLC _beng _cDLC _erda _dES-MaUEC |
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| 050 | 4 |
_aTL671.6 _b.S63 2014 EB |
|
| 082 | 0 | 0 | _a629.134/1 |
| 100 | 1 |
_aSóbester, András _987554 _0Local |
|
| 245 | 1 | 0 |
_aAircraft aerodynamic design : _bgeometry and optimization _cAndrás Sóbester, Alexander Forrester |
| 260 |
_aChichester, West Sussex, United Kingdom _bWiley _c2014 |
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| 300 | _a1 recurso en línea (247 p.) | ||
| 336 |
_aTexto (visual) _btxt _2rdacontent |
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| 337 |
_aelectrónico _bc _2rdamedia |
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| 338 |
_arecurso electrónico _bcr _2rdacarrier |
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| 338 |
_avolume _bnc _2rdacarrier |
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| 490 | 1 | _aAerospace Series | |
| 504 | _aIncludes bibliographical references and index | ||
| 520 |
_a"Optimal aircraft design is impossible without a parametric representation of the geometry of the airframe. We need a mathematical model equipped with a set of controls, or design variables, which generates different candidate airframe shapes in response to changes in the values of these variables. This model's objectives are to be flexible and concise, and capable of yielding a wide range of shapes with a minimum number of design variables. Moreover, the process of converting these variables into aircraft geometries must be robust. Alas, flexibility, conciseness and robustness can seldom be achieved simultaneously.Aircraft Aerodynamic Design: Geometry and Optimization addresses this problem by navigating the subtle trade-offs between the competing objectives of geometry parameterization. It beginswith the fundamentals of geometry-centred aircraft design, followed by a review of the building blocks of computational geometries, the curve and surface formulations at the heart of aircraft geometry. The authors then cover a range of legacy formulations in the build-up towards a discussion of the most flexible shape models used in aerodynamic design (with a focus on lift generating surfaces). The book takes a practical approach and includes MATLAB(r), Python and Rhinoceros(r) code, as well as 'real-life' example case studies.Key features: Covers effective geometry parameterization within the context of design optimization Demonstrates how geometry parameterization is an important element of modern aircraft design Includes code and case studies which enable the reader to apply each theoretical concept either as an aid to understanding or as a building block of their own geometry model Accompanied by a website hosting codes Aircraft Aerodynamic Design: Geometry and Optimization is a practical guide for researchers and practitioners in the aerospace industry, and a reference for graduate and undergraduate students in aircraft design and multidisciplinary design optimization"-- _cProvided by publisher. |
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| 942 |
_2lcc _cLE |
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| 988 | _aEBOOK, EBNETLUEM | ||
| 650 | 7 |
_aAviones _xDiseño y construcción _9138154 _0comprobar BNE19925772719 _2embne |
|
| 700 | 1 |
_aForrester, Alexander I. J. _987555 _0Local |
|
| 856 | 4 | 0 |
_uhttps://search.ebscohost.com/login.aspx?direct=true&scope=site&lang=es&db=nlebk&site=eds-live&AN=855636 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid) |
| 907 |
_a.b12866817 _b10-10-17 _c23-09-15 |
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| 998 |
_am _a_alco _a_vill _b27-05-16 _cm _dz _ea _feng _guik _h0 |
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| 945 |
_aTL671.6 .S63 2014 EB _g1 _ieBOOK _j0 _lmae _o- _pEUR0.00 _q- _r- _sb _t15 _u0 _v0 _w0 _x0 _y.i11557175 _z06-04-17 |
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| 999 |
_c79502 _d79502 _x1 |
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