지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.14 Number.3
- 발행연도
- 2013.9
- 수록면
- 222 - 228 (7page)
이용수
초록· 키워드
오류제보하기
A jetfighter shape modeling method based on design features is researched, to improve the efficiency of shape modeling in the stage of conceptual aircraft design. The aircraft’s general design features and shape parameters, including geometric and position parameters, are described. The coordinate systems of the entire aircraft and its components are defined. As a sample of local shape, a method of inlet intake modeling is introduced. The whole process of the modeling method is proposed. Three examples of different jetfighters are listed, to describe the achievement of basic layout, which includes four main elements. The Fusion of Components can be achieved by regulating the details of the sections of the fuselage. Sample Cases of typical layouts are shown to verify the effectiveness of the proposed method, which provides the basis for further analysis and optimization.
목차
Abstract
1. Introduction
2. Parametric Description of the General Design Features
3. Shape Modeling Method
4. Sample Cases
5. Conclusion
References
참고문헌 (22)
참고문헌 신청
1. [단행본] - Gu, S. F. / 2001 / Aircraft conceptual/preliminary design / Beijing University of Aeronautics and Astronautics Press
2. [단행본] - Raymer, D. P. / 1999 / Aircraft design: a conceptual approach / AIAA Inc
3. [학술지(정기간행물)] - Nicolas, E. A. / 2005 / Framework for Aircraft Conceptual Design and Environmental Performance Studies / AIAA JOURNAL 43 (10) : 2100 ~ 2109
4. [학술대회논문] - Nicolas, A. / 2004 / A Framework for Aircraft Conceptual Design and Environmental Performance Studies / 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization conference
5. [학술대회논문] - Russell, K. D. / 2012 / Parametric Geometry for Propulsion-Airframe Integration / 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
2. [단행본] - Raymer, D. P. / 1999 / Aircraft design: a conceptual approach / AIAA Inc
3. [학술지(정기간행물)] - Nicolas, E. A. / 2005 / Framework for Aircraft Conceptual Design and Environmental Performance Studies / AIAA JOURNAL 43 (10) : 2100 ~ 2109
4. [학술대회논문] - Nicolas, A. / 2004 / A Framework for Aircraft Conceptual Design and Environmental Performance Studies / 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization conference
5. [학술대회논문] - Russell, K. D. / 2012 / Parametric Geometry for Propulsion-Airframe Integration / 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
이 논문의 저자 정보
이 논문과 함께 이용한 논문
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-ECN-0101-2014-550-002838215