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boundary layerAnatomical structure
The explanation of the erosive burning threshold presence has been offered. It is shown that such kind of burning begins at decrease in thickness of the laminar sublayer (in a turbulent boundary layer) below width of the laminar burning zone. The expressions connecting critical (threshold) rate of the blowing stream and critical number of V. N. Vilyunov with properties of fuel and gas formed at its decomposition are obtained. Simple power dependences on blowing stream rate are found for burning rate
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...
ABSTRACT The characteristic of solid propellant burning from the rocket motor static test could be s...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
The elemental theory of concentration limits of slow burning and detonation existence has been offer...
Erosive burning refers to the augmentation of propellant burning rate appears when the velocity of c...
Increasing the velocity of gases inside solid rocket motors with low port-to-throat area ratios, lea...
This paper considers the extensive data and correlations on the erosive burning of solid propellants...
Experimental and computer methods were developed for investigating the combustion phenomena in the p...
Internal ballistics simulations of solid rocket motors have been conducted with the propellant grain...
Calculation of the Admittance Function for a Burning Surface. A thorough analysis of pressure oscil...
A derivation of turbulent flow parameters, combined with data from erosive burning test motors and b...
Two different independent variable forms, a difference form and a ratio form, were investigated for ...
A modified method for prediction of performance of large motors based on erosion constant obtained ...
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...
ABSTRACT The characteristic of solid propellant burning from the rocket motor static test could be s...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
The theory of erosive burning has been constructed front first principles using turbulent boundary l...
The elemental theory of concentration limits of slow burning and detonation existence has been offer...
Erosive burning refers to the augmentation of propellant burning rate appears when the velocity of c...
Increasing the velocity of gases inside solid rocket motors with low port-to-throat area ratios, lea...
This paper considers the extensive data and correlations on the erosive burning of solid propellants...
Experimental and computer methods were developed for investigating the combustion phenomena in the p...
Internal ballistics simulations of solid rocket motors have been conducted with the propellant grain...
Calculation of the Admittance Function for a Burning Surface. A thorough analysis of pressure oscil...
A derivation of turbulent flow parameters, combined with data from erosive burning test motors and b...
Two different independent variable forms, a difference form and a ratio form, were investigated for ...
A modified method for prediction of performance of large motors based on erosion constant obtained ...
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...
ABSTRACT The characteristic of solid propellant burning from the rocket motor static test could be s...
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