VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University9310.18287/1998-6629-2013-0-2(40)-54-60UnknownExperimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel componentsShustovS. A.<p>Candidate of Technical Science</p>
<p>Associate Professor of the Department of Aircraft Engine Theory</p>shustov.st@yandex.ruSamara State Aerospace University18042013122546028042014Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>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.</p>Self-igniting fuel componentsmixing headablation process methodwall boundary flowboundary layercombustion productswall boundary flow temperaturewall boundary flow thicknesswall boundary flow phase compositionСамовоспламеняющиеся компоненты топливасмесительная головкаметод уноса массыпристенокпограничный слойпродукты сгораниятемпература пристенкатолщина пристенкафазовый состав пристенка