추력 노즐 변화에 따른 수소 스크램제트 엔진 특성Investigation on the performance of hydrogen fuel scramjet engine with thrust nozzle variation
- Advisors
- 권세진researcher; Kwon, Se-Jin
- Description
- 한국과학기술원 : 항공우주공학전공,
- Publisher
- 한국과학기술원
- Issue Date
- 2014
- Identifier
- 591866/325007 / 020115211
- Language
- kor
- Description
학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2014.8, [ xiii, 123 p. ]
- Keywords
스크램제트 엔진; Net Thrust; Thrust Nozzle; Supersonic Combustor; Supersonic Intake; Scramjet Engine; 초음속 흡입구; 초음속 연소기; 추력 노즐; 순추력
- Appears in Collection
- AE-Theses_Ph.D.(박사논문)
- Files in This Item
- There are no files associated with this item.
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