Network


Latest external collaboration on country level. Dive into details by clicking on the dots.

Hotspot


Dive into the research topics where Linh Do Duc is active.

Publication


Featured researches published by Linh Do Duc.


international conference on military technologies | 2015

Study of phase behavior of carbon dioxide as the power gas for gas guns

Linh Do Duc; Vladimír Horák; Tomáš Lukáč; Quang Huy Mai

The article is focused on the examination of the phase behavior of carbon dioxide (CO2) utilized as the source of energy to propel the projectile in gas guns technology. The objective is to develop an equilibrium discharge mathematical model for carbon dioxide tanks in order to assume thermodynamic equilibrium states at every point in time throughout discharging under ambient temperature conditions. The speed of sound in a two-phase saturation is taken into consideration for the calculation algorithm. The presented model is solved using the MATLAB environment. An experimental setup has been established for the purpose of verifying the results of solution.


SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE | 2016

DYNAMICS OF KNOCK-OPEN VALVE FOR GAS GUNS POWERED BY CARBON DIOXIDE

Linh Do Duc; Vladimír Horák; Tomáš Lukáč; Roman Vítek; Quang Huy Mai

The paper is focused on the dynamics of knock-open valve used to control the mass flow from a carbon dioxide (CO2) reservoir. The objective is to formulate the mathematical model simulating dynamics of the knock-open valve system for the gas guns powered by carbon dioxide. The equilibrium discharge mathematical model is overviewed, modified and evaluated to obtain the thermodynamic equilibrium states taking place within the reservoir. The problem is solved using MATLAB environment and results of theoretical solution are verified experimentally. Influence of changes in some design parameters of the knock-open valve system to the mass discharge of CO2 within the reservoir is comprehensively examined.


SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE | 2016

EXPERIMENTAL MECHANICAL DEVICE FOR RECOIL SIMUALTION

Tomáš Lukáč; Roman Vítek; Linh Do Duc; Vladimír Horák

The paper deals with the development and testing of the experimental, spring powered mechanical device for the simulation of the gun’s recoil and further for the obtaining the experimental data for the purpose of research and development of the device for gun’s recoil simulation. Several kinds of the present firearm recoil simulation systems and principles of their function are closely described and explained. Measured force diagrams for the experimental mechanical device and for the real assault rifle are presented.


international conference on military technologies | 2017

The internal ballistics of airguns

Linh Do Duc; Vladimír Horák; Roman Vítek; Vladimir V. Kulish

The paper is focused on the development of a thermodynamic mathematical model describing the internal ballistic phenomena, taking place within working chambers of an airgun. The objective is to derive a governing equation modeling the change of gas temperature in a control volume subsuming several incoming and outgoing mass airflow rates. A novel algorithm for solving internal ballistics of all types of airguns is also developed and applied for the case of spring-piston airgun. The mathematical model and solving algorithm are validated and verified experimentally.


international conference on military technologies | 2017

Biomechanical analysis of the shooter-weapon system oscillation

Dung Nguyen Thai; Dung Nguyen Van; Phuc Ta Van; Linh Do Duc

The paper deals with analysis of shooter — weapon system oscillation when firing from a biomechanical point of view. The biomechanical model of shooter arms is developed by taking the muscles and tendons forces into consideration. Linking between shooter and the weapon is treated as elastic and viscose damping. The dynamic model developed for a gas operated submachine gun by applying Lagrange equation of motion has thirteen degrees of freedom. The shooter arms joint stiffness and damping coefficients are experimentally determined. The problem is numerically solved and experimentally verified for the 7.62 mm AKM. The method is able to analyze the shooter — weapon system parameters affecting the gas operated weapon firing stability.


SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE | 2017

DYNAMICS OF RECOIL SIMULATION DEVICE POWERED BY CARBON DIOXIDE

Linh Do Duc; Vladimír Horák; Tomáš Lukáč; Vladimir Kulish

The paper is focused on the dynamics of the recoil simulation device powered by the carbon dioxide (CO2). The objective is to formulate a mathematical model simulating the cylinder pressurization, and the displacement of the recoil simulation device moving part. The CO2 is considered as the real gas. The speed of sound in a two-phase saturation is taken into account for the determination of the critical gas flow rate from the CO2 pressure tank into the cylinder. The problem is solved using the MATLAB environment and results of the theoretical solution are verified experimentally.


ICNPAA 2016 WORLD CONGRESS: 11th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences | 2017

Application of fractional calculus to modeling transient combustion of solid propellants

Vladimir Kulish; Vladimír Horák; Linh Do Duc; Tomáš Lukáč

It was Zel’dovich, who first considered the transient combustion problem of solid propellants. Some more detailed models of that process have been developed afterwards. However, until today, numerical methods remain the prevailing tool for modeling unsteady combustion processes. In this work, it has been demonstrated that at least one of the problems of the unsteady combustion theory, which previously investigated numerically, can be treated analytically by means of fractional calculus. The solution for the unsteady speed of combustion thus derived is then compared with the solution obtained by numerical means in previous studies. The comparison shows a good agreement between those results, especially for small values of time.It was Zel’dovich, who first considered the transient combustion problem of solid propellants. Some more detailed models of that process have been developed afterwards. However, until today, numerical methods remain the prevailing tool for modeling unsteady combustion processes. In this work, it has been demonstrated that at least one of the problems of the unsteady combustion theory, which previously investigated numerically, can be treated analytically by means of fractional calculus. The solution for the unsteady speed of combustion thus derived is then compared with the solution obtained by numerical means in previous studies. The comparison shows a good agreement between those results, especially for small values of time.


ICNPAA 2016 WORLD CONGRESS: 11th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences | 2017

On the possibility to develop an advanced non-equilibrium model of depressurisation in two-phase fluids

Linh Do Duc; Vladimír Horák; Vladimir Kulish; Tomáš Lukáč

Carbon dioxide is widely used as the power gas in the gas guns community due to its ease of handling, storability at room temperature, and high vapor pressure depending only upon temperature, but not a tank size, as long as some liquid carbon dioxide remains in the tank. This high vapor pressure can be used as the pressurant, making it what is referred to as a self-pressurising propellant. However, as a two-phase substance, carbon dioxide does have its drawbacks: (1) vaporization of liquefied CO2 inside a tank when shooting rapidly or a lot causes the tank to get cool, resulting in pressure fluctuations that makes the gun’s performance and accuracy worse, (2) solid carbon dioxide that is also known as dry ice can appear on the output valve of the tank while shooting and it can cause damage or slow the gun’s performance down, if it works its way into some control components, including the barrel of the gun. Hence, it is crucial to obtain a scientific understanding of carbon dioxide behavior and further the...


SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE | 2018

A STUDY ON RECOIL INTENSITY OF THE CO2 POWERED RECOIL SIMULATOR

Linh Do Duc; Vladimír Horák; Roman Vítek; Dung Thai Nguyen


ICNPAA World Congress 2018 | 2018

CHAOTIC BEHAVIOUR OF THE EXACT SOLUTION TO THE NAVIERSTOKES EQUATION: TRANSITION TO TURBULENCE

Vladimír Horák; Vladimir Kulish; Rushikesh Pawar; Linh Do Duc

Collaboration


Dive into the Linh Do Duc's collaboration.

Top Co-Authors

Avatar
Top Co-Authors

Avatar
Top Co-Authors

Avatar
Top Co-Authors

Avatar

Vladimir Kulish

Southern Methodist University

View shared research outputs
Top Co-Authors

Avatar

Quang Huy Mai

Le Quy Don Technical University

View shared research outputs
Top Co-Authors

Avatar

Dung Nguyen Thai

Le Quy Don Technical University

View shared research outputs
Top Co-Authors

Avatar

Dung Nguyen Van

Le Quy Don Technical University

View shared research outputs
Top Co-Authors

Avatar

Phuc Ta Van

Le Quy Don Technical University

View shared research outputs
Top Co-Authors

Avatar

Vladimir V. Kulish

Nanyang Technological University

View shared research outputs
Researchain Logo
Decentralizing Knowledge