공동형 보염기를 갖는 수소연료 스크램제트 연소기의 연소성능Combustion performance of hydrogen fuel scramjet combustor with cavity type flame holder

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Advisors
권세진researcherKwon, Se-Jin
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2013
Identifier
513991/325007  / 020105128
Language
kor
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2013.2, [ xiii, 155 p. ]

Keywords

공동; 다중분사; 단일분사; 스크램제트; 보염기; Scramjet; Single Injection; Staged Injection; Cavity; Flame Holder; Supersonic Combustion; 초음속 연소

URI
http://hdl.handle.net/10203/179653
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=513991&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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