The theory of erosive burning has been constructed front first principles using turbulent boundary layer concepts. It is shown that the problem constitutes one of solution of flame propagation equation for turbulent flow. The final approximate solution for the case of single step overall kinetics reveals the combined effects of fluid mechanics and chemical kinetics. The results obtained from this theory are compared with earlier experimental results. The dependence of erosive burning characteristics on various parameters has been elucidated
This paper addresses erosive burning of a cylindrical composite propellant grain. Equations governin...
Among various aspects dealing with the influence of flow structure on the combustion characteristics...
A derivation of turbulent flow parameters, combined with data from erosive burning test motors and b...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
Erosive burning refers to the augmentation of propellant burning rate appears when the velocity of c...
The explanation of the erosive burning threshold presence has been offered. It is shown that such ki...
Increasing the velocity of gases inside solid rocket motors with low port-to-throat area ratios, lea...
Four erosive burning models, equations (11) to (14). are developed in this work by using a power law...
The paper studies the features of the erosive burning of complex configurations of solid propellant ...
To acquire the erosive characteristics of two-channel combustion chambers, a quasi-one-dimensional i...
Erosive burning changes the burning rate of solid rocket propellants which can normally be approxima...
Experimental and computer methods were developed for investigating the combustion phenomena in the p...
Using the theory of gas dynamics and heat transfer from a turbulent gas flow to the burning surface ...
ABSTRACT The characteristic of solid propellant burning from the rocket motor static test could be s...
This paper considers the extensive data and correlations on the erosive burning of solid propellants...
This paper addresses erosive burning of a cylindrical composite propellant grain. Equations governin...
Among various aspects dealing with the influence of flow structure on the combustion characteristics...
A derivation of turbulent flow parameters, combined with data from erosive burning test motors and b...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
Erosive burning refers to the augmentation of propellant burning rate appears when the velocity of c...
The explanation of the erosive burning threshold presence has been offered. It is shown that such ki...
Increasing the velocity of gases inside solid rocket motors with low port-to-throat area ratios, lea...
Four erosive burning models, equations (11) to (14). are developed in this work by using a power law...
The paper studies the features of the erosive burning of complex configurations of solid propellant ...
To acquire the erosive characteristics of two-channel combustion chambers, a quasi-one-dimensional i...
Erosive burning changes the burning rate of solid rocket propellants which can normally be approxima...
Experimental and computer methods were developed for investigating the combustion phenomena in the p...
Using the theory of gas dynamics and heat transfer from a turbulent gas flow to the burning surface ...
ABSTRACT The characteristic of solid propellant burning from the rocket motor static test could be s...
This paper considers the extensive data and correlations on the erosive burning of solid propellants...
This paper addresses erosive burning of a cylindrical composite propellant grain. Equations governin...
Among various aspects dealing with the influence of flow structure on the combustion characteristics...
A derivation of turbulent flow parameters, combined with data from erosive burning test motors and b...