Chung et al., 2016 - Google Patents
Dynamic characteristics of open-type swirl injector with varying geometryChung et al., 2016
- Document ID
- 13483224748124304265
- Author
- Chung Y
- Kim H
- Jeong S
- Yoon Y
- Publication year
- Publication venue
- Journal of Propulsion and Power
External Links
Snippet
Combustion instabilities in a liquid rocket engine are generated by coupling between the heat release oscillations and the acoustic pressure oscillations in the combustion chamber. These instabilities from the combustion chamber can affect the injector and the feed line …
- 239000007788 liquid 0 abstract description 79
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
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