An Axisymmetrical Study on the Secondary Reaction of Launch Vehicle Turbine Exhaust Gas Using the Detailed Chemistry Model (상세 화학반응 모델을 이용한 발사체 터빈 배기가스의 이차연소 해석의 축대칭 해석)
-
- Proceedings of the Korean Society of Propulsion Engineers Conference
- /
- 2011.11a
- /
- pp.857-862
- /
- 2011