| Autor: |
Brandon Kan, David P. Stechmann, Brent Justice, Stephen D. Heister, Dasheng Lim |
| Rok vydání: |
2015 |
| Předmět: |
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| Zdroj: |
51st AIAA/SAE/ASEE Joint Propulsion Conference. |
| DOI: |
10.2514/6.2015-3767 |
| Popis: |
A series of experiments has been performed to study the transient response of a liquid injector to a transverse detonation wave. Using an optically accessible test article and a high speed camera, images were captured at 80,000 frames per second to reveal the dynamic nature of a water column’s response as a detonation wave traverses the injector orifice exit. High frequency pressure measurements were collected to be used as input for a one-dimensional lumped parameter computational model developed as a quick method of generating preliminary design parameters for an injector used in a pressure gain combustor. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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