dcterms:abstract
  • The cycle analysis of the tip jet rotorcraft engine system was performed. From the basic characteristics of the tip jet rotorcraft, the design requirements of the tip jet power system was established. Three kinds of power systems such as a turbojet, a turbofan and a turboprop engines were studied for the tip jet power system. From the performance analysis, we could understand characteristics of the each engine system for the tip jet rotorcraft (xsd:string)
  • 팁 제트 헬리콥터 엔진시스템의 동력장치에 대한 사이클 해석을 수행하였다. 팁 제트 헬리콥터의 개념으로부터 설계요구조건을 도출하였다. 터보제트, 터보팬, 터보프롭을 이용하여 팁제트 동력장치의 적용 가능성을 연구하였으며, 성능해석결과 각각의 엔진에 대한 팁 제트 헬리콥터의 작동특성을 이해할 수 있었다 (xsd:string)
dcterms:accessRights
dcterms:alternative
  • Conceptual study of the propulsion system for the combined rotorcraft (xsd:string)
nlon:antecedentSource
  • born digital (xsd:string)
nlon:audienceNote
  • 일반이용자 (xsd:string)
nlon:bibliography
  • 참고문헌: p. 330 (xsd:string)
dc:creator
  • 김선미 (xsd:string)
  • 김혜민 (xsd:string)
  • 양계병 (xsd:string)
  • 최성만 (xsd:string)
dcterms:creator
nlon:datePublished
  • 2021-01-12T14:52:20 (xsd:dateTime)
bibframe:extent
  • 3 p (xsd:string)
dc:format
  • application/pdf (xsd:string)
nlon:genre
  • 학술논문 (xsd:string)
nlon:holdingInstitution
  • 국립중앙도서관 (xsd:string)
dcterms:identifier
  • http://www.kspe.org (xsd:string)
dcterms:isPartOf
nlon:keyword
  • Tip jet rotorcraft, 팁 제트 헬리콥터, Cycle Analysis, 성능해석, Turbojet, 터보제트, Turbofan, 터보팬, Turboprop, 터보프롭 (xsd:string)
rdfs:label
  • 복합형헬기 추진기관 개념연구 (xsd:string)
nlon:languageNote
  • 영어 요약 있음 (xsd:string)
nlon:medium
  • 전자자료(Application) (xsd:string)
nlon:newsPosition
  • p. 328-330 (xsd:string)
nlon:publicationPlace
  • 한국 (xsd:string)
nlon:relatedParts
  • 제45회 (xsd:string)
nlon:restriction
  • 국립중앙도서관 공개 (xsd:string)
dcterms:title
  • 복합형헬기 추진기관 개념연구 (xsd:string)
nlon:titleOfHostItem
  • Proceedings of the ... KSPE conference (xsd:string)
  • 한국추진공학회 ...학술대회논문초록집 (xsd:string)
rdf:type
nlon:typeOfResource
nlon:uci
  • G701:A-00116726184 (xsd:string)