Prediscovery in the field of the whirlwind reverse-flow type combustion chambers making

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Abstract

The scheme of the whirlwind reverse-flow type combustion chamber generalized model is submitted. The parametric equation connecting thermodynamic and gasdynamic properties of main combustion chamber burners units, permitting to receive integral characteristics of combustion chamber probed version and to evaluate effect of each basic elements making a combustion chamber, on its output parameters ful fillment is received.

About the authors

Rybinsk State Aviation Technological Academy

Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation

Rybinsk State Aviation Technological Academy

Email: sadohina@ssau.ru
Russian Federation

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