An experimental method was used to determine the intensity of turbulence and the Lagrangian correlation coefficient in a GH2-GOX rocket combustion chamber. The method consisted of injecting a tracer gas at an upstream point on the centerline of the combustion chamber while taking gas samples along a
โฆ LIBER โฆ
Thermal fluxes in combustion chamber walls in the detonation and turbulent combustion modes
โ Scribed by F. A. Bykovskii
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 1991
- Tongue
- English
- Weight
- 569 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0010-5082
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