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Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
- Authors: Shustov S.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 12, No 2 (2013)
- Pages: 54-60
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/93
- DOI: https://doi.org/10.18287/1998-6629-2013-0-2(40)-54-60
- ID: 93
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Abstract
The paper presents a method of experimental investigation of physical processes taking place in the formation of a wall boundary flow. The object of investigation is described. The results of the experimental research are presented. They are related to such parameters as changes in the thickness, temperature and phase composition of the wall boundary flow. The results of comparing the thickness of the wall boundary flow and that of the boundary layer along the combustion chamber are given.
About the authors
S. A. Shustov
Samara State Aerospace University
Author for correspondence.
Email: shustov.st@yandex.ru
Candidate of Technical Science
Associate Professor of the Department of Aircraft Engine Theory
Russian FederationReferences
- Метод определения профилей состава и температуры высокотемпературных газовых потоков [Текст] / В.Н. Градов, В.Е. Нигодюк С.А. Шустов [и др.] // Инженерно-физический журнал, 1980. - Т.XXXVIII. - С. 853-858.
- Нигодюк, В.Е. Исследование закономерностей жидкофазного взаимодействия компонентов СЖРТ [Текст] / В.Е. Нигодюк, А.В Сулинов // Вестник СГАУ, 2009. - Ч.2. - №3 (19). - С. 316-320.
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