Add to ORKGThe current work predicts the combustion characteristics of a solid rocket motor especially the flow in the nozzle part. The simulation work is done using computational fluids dynamic (CFD) software. The volume mesh was built in one quarter of the nozzle to reduce time for calculation. The same nozzle is also created with different mesh sizes for grid dependency check. All the rocket parameter is obtained from the theoretical design of rocket motor based on basic nozzle design. The simulation result in CFD is compared to the theoretical calculations and it shows that the modelling of rocket nozzle results shows good agreement with the theoretical ones. Parametric study on the nozzle was conducted. The results show that the best nozzle confi...
A computational thermo-fluid-dynamic model of the hybrid rocket internal ballistics has been develop...
The blast tube flowfield of a solid rocket motor is explored numerically by solving 3-D RANS equatio...
A numerical model for analysis of thermal and mechanical loads of a rocket motor has been developed....
A Solid propellant Retro Rocket Motor with a C-D Nozzle is analyzed using Ansys Fluent 17.1 .Steady ...
Integral rocket ramjet (IRR) type propulsion systems have many advantages over conventional solid ro...
A numerical code that simulates combustion phenomena occurring in a solid rocket motor is developed ...
The ability of a propulsion system is very crucial for the capability of a missile or a rocket syste...
There was a lot of study on Solid Rocket Motor (SRM) based solid propellant. This project focus on a...
A compound-compressible flow nozzle can be used to augment the thrust generated by a rocket engine b...
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid roc...
Traditionally, Solid Rocket Motor (SRM) internal ballistic performance has been analyzed and predict...
The object of the investigations is the nozzles of the solid propellant rocket engine. Experimental ...
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid roc...
The thrust produced by a rocket motor is mainly dependent upon the expansion of the product gases th...
This paper focuses on the role of CFD in developing rocket propulsion system by simulating major dev...
A computational thermo-fluid-dynamic model of the hybrid rocket internal ballistics has been develop...
The blast tube flowfield of a solid rocket motor is explored numerically by solving 3-D RANS equatio...
A numerical model for analysis of thermal and mechanical loads of a rocket motor has been developed....
A Solid propellant Retro Rocket Motor with a C-D Nozzle is analyzed using Ansys Fluent 17.1 .Steady ...
Integral rocket ramjet (IRR) type propulsion systems have many advantages over conventional solid ro...
A numerical code that simulates combustion phenomena occurring in a solid rocket motor is developed ...
The ability of a propulsion system is very crucial for the capability of a missile or a rocket syste...
There was a lot of study on Solid Rocket Motor (SRM) based solid propellant. This project focus on a...
A compound-compressible flow nozzle can be used to augment the thrust generated by a rocket engine b...
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid roc...
Traditionally, Solid Rocket Motor (SRM) internal ballistic performance has been analyzed and predict...
The object of the investigations is the nozzles of the solid propellant rocket engine. Experimental ...
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid roc...
The thrust produced by a rocket motor is mainly dependent upon the expansion of the product gases th...
This paper focuses on the role of CFD in developing rocket propulsion system by simulating major dev...
A computational thermo-fluid-dynamic model of the hybrid rocket internal ballistics has been develop...
The blast tube flowfield of a solid rocket motor is explored numerically by solving 3-D RANS equatio...
A numerical model for analysis of thermal and mechanical loads of a rocket motor has been developed....