The influence of combustion efficiency on the characteristics of ramjets


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Abstract

Methods for determining the combustion efficiency, thermodynamics parameters of propellants, and characteristics of ramjets are analyzed. Energetic and multizone models taking into account various physical processes of incomplete combustion are considered. An approach based on comparison of the combustion efficiency evaluated by different models is developed, and recommendations on their application are given. The results and mathematical models presented can be used in numerical computational and experimental studies of the working processes in ramjets.

About the authors

I. S. Aver’kov

Baranov Central Institute of Aviation Motor Development

Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116

V. Yu. Aleksandrov

Baranov Central Institute of Aviation Motor Development; Moscow Institute of Physics and Technology

Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116; Dolgoprudnyi, Moscow oblast, 141701

K. Yu. Aref’ev

Baranov Central Institute of Aviation Motor Development; Moscow Institute of Physics and Technology; Bauman Moscow State Technical University

Author for correspondence.
Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116; Dolgoprudnyi, Moscow oblast, 141701; Moscow, 105005

A. V. Voronetskii

Bauman Moscow State Technical University

Email: arefyev@ciam.ru
Russian Federation, Moscow, 105005

O. V. Gus’kov

Baranov Central Institute of Aviation Motor Development; Moscow Institute of Physics and Technology

Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116; Dolgoprudnyi, Moscow oblast, 141701

A. N. Prokhorov

Baranov Central Institute of Aviation Motor Development; Moscow Institute of Physics and Technology

Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116; Dolgoprudnyi, Moscow oblast, 141701

L. S. Yanovskii

Baranov Central Institute of Aviation Motor Development

Email: arefyev@ciam.ru
Russian Federation, Moscow, 111116

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