• 제목/요약/키워드: 다학제 최적설계

검색결과 3건 처리시간 0.02초

반응면 기법을 이용한 초음속 전투기 날개의 다학제간 다점 설계 (Multidisciplinary Multi-Point Design Optimization of Supersonic fighter Wing Using Response Surface Methodology)

  • 김유신;김재무
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2004년도 추계 학술대회논문집
    • /
    • pp.173-176
    • /
    • 2004
  • In this study, the multidisciplinary aerodynamic-structural optimal design is carried out for the supersonic fighter wing. Through the aeroelastic analyses of the various candidate wings, the aerodynamic and structural performances are calculated such as the lift coefficient, the drag coefficient and the deformation of the wing. In general, the supersonic fighter is maneuvered under the various flight conditions and those conditions must be considered all together during the design process. The multi-point design, therefore, is deemed essential. For this purpose, supersonic dash, long cruise range and high angle of attack maneuver are selected as representative design points. Based on the calculated performances of the candidate wings, the response surfaces for the objectives and constraints are generated and the supersonic fighter wing is designed for better aerodynamic performances and less weights than the baseline. At each design point, the single-point design is performed to obtain better performances. Finally, the multi-point design is performed to improve the aerodynamic and structural performances for all design points. The optimization results of the multi-point design are compared with those of the single-point designs and analyzed in detail.

  • PDF

비행체 RCS 예측을 위한 CEM 기법 연구 (Development of a Computational Electromagnetics Code for Radar Cross Section Calculations of Flying Vehicles)

  • 명노신;조태환
    • 한국항공우주학회지
    • /
    • 제33권4호
    • /
    • pp.1-6
    • /
    • 2005
  • 적대적 환경에서 임무를 수행하는 비행체의 레이다 포착에 관련된 스텔스 기술이 주요 설계 문제로 부각되고 있다. 레이다 회피 기능을 증대시키는 방안들을 분석하기 위해서는 Maxwell 방정식을 해석하는 기법이 필요한데, 본 연구에서는 기본 수치기법으로 다학제 최적설계 연구에 적합한 CFD 기법을 이용하였다. 시간 영역 전자기장 데이터를 DFFT 알고리즘을 이용하여 주파수 영역으로 변환한 후, 근방-원방 변환에 기초한 Green 함수 관계식을 사용하여 RCS 특성을 예측하였다. 검증을 위해 완전전도 실린더 주위 TE 모드를 고려하였으며, CFD 기법을 원용한 CEM 코드의 가능성을 확인하기 위해 비행체 날개단면 주위의 전자기 산란 현상을 계산하였다.

심해저 채광로봇 기술개발을 위한 Verification & Validation의 적용 (Application of Verification & Validation for deepsea mining robot technology development)

  • 성기영;조수길;오재원;여태경;홍섭;김형우
    • 한국산업융합학회 논문집
    • /
    • 제22권6호
    • /
    • pp.689-702
    • /
    • 2019
  • This paper deals with the verification of the functions about mining robot, which is the system for developing deep seabed resources by applying V&V(verification and validation). In order to overcome water pressure of 500 bar and to travel on soft ground, and to operate in deep sea environment with bad conditions, it is necessary to develop a robot that can satisfy various deepsea conditions. A mining robot has been developed based on simulation based design and Multidisciplinary design optimization. In order to verify the developed robot, lab test and real sea test should be performed for various marine environment conditions. There are too many requirements to consider, such as space, time, cost, personnel, and environment to do performance test. So it is costly and time consuming for developing robot. In order to solve this problems, V&V technique was applied to mining robot. The stages of mining robot design, fabrication and commission were verified.