Solid Rocket Motor Grid Generation and CFD for Internal Ballistics Analysis

2005 ◽  
Author(s):  
Jonathan French ◽  
James Tullos
Keyword(s):  
Grid Generation ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Internal Ballistics ◽  
Solid Rocket

Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver

2022 ◽  
Author(s):  
Griffin A. DiMaggio ◽  
Roy J. Hartfield ◽  
Joseph Majdalani ◽  
Vivek Ahuja
Keyword(s):  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Internal Ballistics ◽  
Solid Rocket

scholarly journals Solid rocket motor internal ballistics using an enhanced surface-vorticity panel technique

2021 ◽  
Vol 33 (10) ◽  
pp. 103613
Author(s):  
Griffin A. DiMaggio ◽  
Roy J. Hartfield ◽  
Joseph Majdalani ◽  
Vivek Ahuja
Keyword(s):  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Internal Ballistics ◽  
Solid Rocket ◽  
Enhanced Surface

scholarly journals Solid Rocket Motor Internal Ballistics Simulation Using Three-Dimensional Grain Burnback

2007 ◽  
Vol 23 (3) ◽  
pp. 575-584 ◽  
Author(s):  
Michael A. Willcox ◽  
M. Quin Brewster ◽  
K. C. Tang ◽  
D. Scott Stewart ◽  
Igor Kuznetsov
Keyword(s):  
Three Dimensional ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Internal Ballistics ◽  
Solid Rocket

Numerical Study of the Effects of Longitudinal Acceleration on Solid Rocket Motor Internal Ballistics

1992 ◽  
Vol 114 (3) ◽  
pp. 404-410 ◽  
Author(s):  
J. J. Gottlieb ◽  
D. R. Greatrix
Keyword(s):  
Numerical Study ◽  
Equations Of Motion ◽  
Rocket Motor ◽  
Rate Equations ◽  
Solid Rocket Motor ◽  
Two Phase ◽  
Internal Ballistics ◽  
Solid Propellant Rocket ◽  
Solid Rocket ◽  
The One

The internal ballistics of a solid-propellant rocket motor subjected to both constant and oscillatory longitudinal accelerations are studied. The one-dimensional time-dependent equations of motion governing the unsteady two-phase core flow in the accelerating motor chamber and nozzle are solved numerically by using the random-choice method, along with pressure-dependent and crossflow-dependent burning-rate equations for propellant combustion. A constant forward acceleration produces negligible effects, whereas longitudinal motor vibrations near the natural frequency of waves criss-crossing the length of the motor chamber can produce large but bounded oscillatory motor-chamber pressures.

Sign in / Sign up

Export Citation Format

Share Document