Numerical Exploration of Solid Rocket Motor Blast Tube Flow Field

2013 ◽  
Vol 63 (6) ◽  
pp. 616-621 ◽  
Author(s):  
Afroz Javed ◽  
P. Sinha ◽  
Debasis Chakraborty
Keyword(s):  
Flow Field ◽  
Rocket Motor ◽  
Tube Flow ◽  
Solid Rocket Motor ◽  
Numerical Exploration ◽  
Solid Rocket

scholarly journals Impact of the Surface Morphology on the Combustion of Simulated Solid Rocket Motor

2015 ◽  
Vol 2015 ◽  
pp. 1-11
Author(s):  
Abdelkarim M. Hegab ◽  
Hani Hussain Sait ◽  
Ahmad Hussain
Keyword(s):  
Flow Field ◽  
Surface Morphology ◽  
Aluminum Powder ◽  
Combustion Surface ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Resonance Frequencies ◽  
Wide Range ◽  
Solid Rocket ◽  
The Impact

An advanced and intensive computational solution development is integrated with an asymptotic technique, to examine the impact of the combustion surface morphology on the generated rotational flow field in a solid rocket chamber with wide ranges of forcing frequencies. The simulated rectangular chamber is closed at one end and is open at the aft end. The upper and lower walls are permeable to allow steady and unsteady injected air to generate internal flow mimicking the flow field of the combustion gases in real rocket chamber. The frequencies of the unsteady injected flow are chosen to be very close or away from the resonance frequencies of the adapted chamber. The current study accounts for a wide range of wave numbers that reflect the complexity of real burning processes. Detailed derivation for Navier-Stokes equations at the four boundaries of the chamber is introduced in the current study. Qualitative comparison is performed with recent experimental work carried out on a two-inch hybrid rocket motor using a mixture of polyethylene and aluminum powder. The higher the percentage of aluminum powder in the mixture, the more the corrugations of the combustion surface. This trend is almost similar to the computational and analytical results of a simulated solid rocket chamber.

Numerical Simulation of a Dual Pulse Solid Rocket Motor Flow Field

2012 ◽  
Vol 62 (6) ◽  
pp. 369-374 ◽  
Author(s):  
Afroz Javed ◽  
P. Manna ◽  
Debasis Chakraborty
Keyword(s):  
Numerical Simulation ◽  
Flow Field ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Solid Rocket

scholarly journals Numerical Study on Response Characteristics of Solid Rocket Pintle Motor

2019 ◽  
Author(s):  
Jeevan Sapkota ◽  
Yi Hua Xu ◽  
Hai Jun Sun
Keyword(s):  
Flow Field ◽  
Combustion Chamber ◽  
Total Pressure ◽  
Numerical Study ◽  
Rocket Motor ◽  
Chamber Pressure ◽  
Head Model ◽  
Solid Rocket Motor ◽  
Rapid Changes ◽  
Solid Rocket

Pintle technology is currently a versatile technology used in a solid rocket motor (SRM) to control the desired thrust by changing the nozzle throat area, while effectively controlling the chamber pressure at the same time. The sudden movement of the pintle can induce rapid changes in the flow field and the occurrence of pressure oscillations inside the combustion chamber. The analysis of such rapid changes is essential to design an efficient controllable pintle rocket motor for a better thrust regulation. Two-dimensional axisymmetric models with mesh generation and required boundary condition were designed to analyze the effects of three different pintle head shape models in SRM thrust regulation effect. Dynamic mesh method was used with specific velocity for moving plug/pintle in the numerical analysis of SRM thrust regulation. The effects of different pintle head models on the flow field, combustion chamber pressure, mass-flow rate, thrust and Mach number were investigated. According to the analysis of total pressure response time, the simulation data revealed that circular pintle head model responded faster among three different models. According to the thrust effect, parabolic pintle has the maximum value of thrust and the greatest total pressure recovery coefficient among all pintle head models.

Coupled Analysis the Segmented SRM Internal Flow Field with Influence of Inhibitor Deformation

2012 ◽  
Vol 452-453 ◽  
pp. 1346-1350
Author(s):  
Shuang Wu Gao ◽  
Hong Fu Qiang ◽  
Wei Zhou ◽  
Peng Peng Wu
Keyword(s):  
Flow Field ◽  
Fluid Structure Interaction ◽  
Internal Flow ◽  
Rocket Motor ◽  
Coupled Analysis ◽  
Solid Rocket Motor ◽  
Fluid Structure ◽  
Large Eddy Simulation Model ◽  
Structure Interaction ◽  
Solid Rocket

The coupled influence between structure and internal flow field will make the pressure oscillation during working process of the solid rocket motor. This coupled effect will bring the dynamic press on the payload and extremely destroyed the payload. For researching the influence of internal flow field by the deformation of inhibitor, the parallel fluid structure interaction method with the large eddy simulation model was used to analyze the solid rocket motor with segments. The results show that the deformation of inhibitor will influence the internal flow field parameter’s distribution and enhance the pressure frequency and amplitude remarkably. The partitioned method could solution the fluid structure interaction problems in the segmented solid rocket motor properly.

scholarly journals Turbulent Flow Characteristics in a Model of a Solid Rocket Motor Chamber with Sidewall Mass Injection and End-Wall Disturbance

2021 ◽  
Vol 2021 ◽  
pp. 1-17
Author(s):  
F. A. Albatati ◽  
A. M. Hegab ◽  
M. A. Rady ◽  
A. A. Abuhabaya ◽  
S. M. El-Behery
Keyword(s):  
Flow Field ◽  
Turbulent Flow ◽  
Stokes Equations ◽  
Numerical Study ◽  
Rocket Motor ◽  
Staggered Grid ◽  
Computational Time ◽  
Solid Rocket Motor ◽  
Solid Rocket ◽  
End Wall

The present analytical, numerical, and experimental investigations are performed to study the flow field in acoustically simulated solid rocket motor (SRM) chamber geometry. The computational solution is carried out for a high Reynolds number and low Mach number internal flows driven by sidewall mass addition in a long chamber with end-wall disturbances. This kind of flow (transient, weakly viscous, and contains vorticity) have several features in common with a turbulent flow field. The numerical study is performed by solving the unsteady Reynolds-averaged Navier–Stokes equations along with the energy equation using the control volume approach based on a staggered grid system. The v2-f turbulence model has been implemented in the current study. A comparison of the SIMPLE and PISO algorithms showed that both algorithms provide identical results, and the computational time using the PISO algorithm is higher by about 6% than the corresponding value of the SIMPLE algorithm. A fair agreement has been obtained between the numerical, analytical, and experimental results. Moreover, the results showed that the complex turbulent internal flow patterns are induced inside the chamber due to the strong interaction of the sidewall injection with the traveling acoustic waves. Such a complex internal structure is shown to be dependent on the piston frequency and sidewall mass flux. The current study, for the first time, emphasizes the acoustic-fluid dynamics interaction mechanism and the accompanying unsteady rotational fields along with the effect of the generated turbulence on the unsteady vorticity and its impact on the real burning rate.

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