소장자료
LDR | 02948cam a2200289 a 4500 | ||
001 | 0093776448▲ | ||
005 | 20180521070307▲ | ||
008 | 140715s2015 enka b 001 0 eng c▲ | ||
010 | ▼a2014026821▲ | ||
020 | ▼a9780470662571 (hbk.)▲ | ||
035 | ▼a(KERIS)REF000017494414▲ | ||
040 | ▼aDLC▼beng▼cDLC▼dDLC▼d221016▲ | ||
042 | ▼apcc▲ | ||
050 | 0 | 0 | ▼aTL671.6▼b.S58 2015▲ |
082 | 0 | 0 | ▼a629.134/1▼223▲ |
090 | ▼a629.1341▼bS677a▲ | ||
100 | 1 | ▼aSóbester, András.▲ | |
245 | 1 | 0 | ▼aAircraft aerodynamic design :▼bgeometry and optimization /▼cAndrás Sóbester and Alexander I J Forrester.▲ |
260 | ▼aChichester :▼bJohn Wiley & Sons Ltd,▼c2015.▲ | ||
300 | ▼axv, 246 p. :▼bill. ;▼c26 cm.▲ | ||
490 | 0 | ▼aAerospace series▲ | |
504 | ▼aIncludes bibliographical references (p. 239-241) 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"--Provided by publisher.▲ | ||
650 | 0 | ▼aAirframes.▲ | |
650 | 0 | ▼aAerodynamics.▲ | |
700 | 1 | ▼aForrester, Alexander I. J.▲ | |
999 | ▼a경동욱▼c김미선▲ |
Aircraft aerodynamic design :geometry and optimization
자료유형
국외단행본
서명/책임사항
Aircraft aerodynamic design : geometry and optimization / András Sóbester and Alexander I J Forrester.
발행사항
Chichester : John Wiley & Sons Ltd , 2015.
형태사항
xv, 246 p. : ill. ; 26 cm.
총서사항
서지주기
Includes bibliographical references (p. 239-241) and index.
요약주기
"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"--Provided by publisher.
ISBN
9780470662571 (hbk.)
청구기호
629.1341 S677a
소장정보
예도서예약
서서가에없는책 신고
보보존서고신청
캠캠퍼스대출
우우선정리신청
배자료배달신청
문문자발송
출청구기호출력
학소장학술지 원문서비스
등록번호 | 청구기호 | 소장처 | 도서상태 | 반납예정일 | 서비스 |
---|
북토크
자유롭게 책을 읽고
느낀점을 적어주세요
글쓰기
느낀점을 적어주세요
청구기호 브라우징
관련 인기대출 도서