인력비행기 스카이 러너 설계.제작.비행

The Design, Construction and Flight of Human Powered Aircraft Sky Runner

  • 이기영 (해군사관학교 기계조선공학과) ;
  • 최성옥 (공군사관학교 항공우주공학과) ;
  • 오장근 (한국신기술연구소)
  • 투고 : 2010.04.26
  • 심사 : 2010.07.23
  • 발행 : 2010.08.05

초록

With the financial sponsorship of FKI and six other companies, the design and construction of the human powered aircraft Sky Runner has been begun to design in December of 2008. And it flew in late December of 2009. The original design configuration was continuously modified in response to test results as a 30.36m span, $35.25m^2$ wing area, 26.0 aspect ratio and 39.8kg of empty weight. Although, we have made only 150m flight flying a few seconds so far however, it will contribute to the research of ultra-light and long duration flying planes. A brief review of some design features, wing layout, prop design, fabrication and flight test results are presented.

키워드

참고문헌

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