Numerical Analysis of Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation

Author(s):  
Toru Shimada ◽  
Masumi Sekiguchi ◽  
Nobuhiro Sekino
AIAA Journal ◽  
2007 ◽  
Vol 45 (6) ◽  
pp. 1324-1332 ◽  
Author(s):  
Toru Shimada ◽  
Masumi Sekiguchi ◽  
Nobuhiro Sekino

1999 ◽  
Author(s):  
Tae-Seong Roh ◽  
Fred Culick ◽  
Norman Cohen ◽  
Robert Beddini

2012 ◽  
Vol 490-495 ◽  
pp. 2290-2294
Author(s):  
Wei Ping Tian ◽  
Chun Guang Wang ◽  
Cong Chen ◽  
De Min Yang

To achieve engineering application of pulse motor as soon as possible,designed a soft pulse separation device(PSD), numerical simulated its process of bearing pressure and turning on,used the XFEM to simulate its failure form,got strain and stress distribution,found the bearing capability and failure form of the structure of soft PSD was reliable;Designed a few of verification monomial tests,verified the accuracy of simulation,proved that its bearing capability and failure form satisfied with design requirements,could be applied to pulse motor.The simulation technique,test method and conclusion are useful for designing pulse solid rocket motor configuration.


2011 ◽  
Vol 48 (1) ◽  
pp. 103-109 ◽  
Author(s):  
Qiao Zhang ◽  
Jun-wei Li ◽  
Wei-chen Wang ◽  
Ning-fei Wang

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