Development of Helicopter Design and Analysis Program for Helicopter Conceptual Design

헬리콥터 개념설계를 위한 설계 및 분석 프로그램 개발

  • 고강명 (서울대학교 기계항공공학부) ;
  • 강승온 (서울대학교 기계항공공학부) ;
  • 김상훈 (서울대학교 기계항공공학부) ;
  • 이동호 (서울대학교 기계항공공학부) ;
  • 장용진 (한국항공우주산업(주) KHP사업부 기체설계담당 비행조종팀) ;
  • 최원 (한국항공우주산업(주) KHP사업부 기체설계담당 비행조종팀) ;
  • 황유상 (한국항공우주산업(주) KHP사업부 기체설계담당 비행조종팀) ;
  • 김철호 (한국항공우주산업(주) KHP사업부 기체설계담당 비행조종팀)
  • Published : 2007.05.30

Abstract

It is necessary a simple helicopter design and performance analysis program for a stage of helicopter conceptual design. To meet that needs, we have developed a program which is simply used to estimate helicopter configuration and performance. The program developed by this study is composed of Requirement, Mission profile Analysis, Size, Aerodynamic, Trim, Propulsion, Weight, and Performance modules, and each modules carry out operations for a given flight condition. In this study, we validate this analysis program in 9,500 1bs and 22,000 1bs helicopters and estimate design configuration and performance of 16,000 1b helicopter. And We can use this program to optimization process for Helicopter MDO framework.

Keywords