Parametric Study on Solid Rocket Motor Ignition Transient and Pressure Oscillations Onset

2015 ◽  
Vol 31 (4) ◽  
pp. 1117-1126 ◽  
Author(s):  
M. Di Giacinto ◽  
E. Cavallini ◽  
B. Favini ◽  
J. Steelant
Keyword(s):  
Parametric Study ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Pressure Oscillations ◽  
Solid Rocket

Variable Fuel Grains Burn Velocities to Reduce Solid-Rocket-Motor Pressure Oscillations

2015 ◽  
Vol 31 (1) ◽  
pp. 342-351 ◽  
Author(s):  
Jérôme Anthoine ◽  
Patrick Jézéquel ◽  
Michel Prévost ◽  
Pierre Prévot ◽  
Grégoire Casalis
Keyword(s):  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Pressure Oscillations ◽  
Solid Rocket

Computational Fluid Dynamics Simulation of Combustion Instability in Solid Rocket Motor : Implementation of Pressure Coupled Response Function

2016 ◽  
Vol 66 (3) ◽  
pp. 216 ◽  
Author(s):  
S. Saha ◽  
D. Chakraborty
Keyword(s):  
Fluid Dynamics ◽  
Growth Rate ◽  
Computational Fluid Dynamics ◽  
Response Function ◽  
Combustion Instability ◽  
Rocket Motor ◽  
Dynamics Simulation ◽  
Solid Rocket Motor ◽  
Pressure Oscillations ◽  
Solid Rocket

<p class="NomenclatureClauseTitle">Combustion instability in solid propellant rocket motor is numerically simulated by implementing propellant response function with quasi steady homogeneous one dimensional formulation. The convolution integral of propellant response with pressure history is implemented through a user defined function in commercial computational fluid dynamics software. The methodology is validated against literature reported motor test and other simulation results. Computed amplitude of pressure fluctuations compare closely with the literarture data. The growth rate of pressure oscillations of a cylindrical grain solid rocket motor is determined for different response functions at the fundamental longitudinal frequency. It is observed that for response function more than a critical value, the motor exhibits exponential growth rate of pressure oscillations.</p>

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