Email this article Modified combustion efficiency curve for high-velocity model combustors integrated with the inlet
- Authors: Aleksandrov V.Y.1, Kukshinov N.V.1
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Affiliations:
- Baranov Central Institute of Aviation Motors
- Issue: Vol 52, No 3 (2016)
- Pages: 281-285
- Section: Article
- URL: https://journals.rcsi.science/0010-5082/article/view/152495
- DOI: https://doi.org/10.1134/S0010508216030047
- ID: 152495
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Abstract
The method of obtaining combustion efficiency curves for fuel mixtures proposed by Annushkin is modified on the basis of data of high-altitude tests of high-velocity combustors integrated with the inlet. The combustion efficiency curve of a hydrocarbon–air mixture obtained in this study can be applied for design of high-velocity combustors.
About the authors
V. Yu. Aleksandrov
Baranov Central Institute of Aviation Motors
Author for correspondence.
Email: kukshinov@ciam.ru
Russian Federation, Moscow, 111116
N. V. Kukshinov
Baranov Central Institute of Aviation Motors
Email: kukshinov@ciam.ru
Russian Federation, Moscow, 111116
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