DocumentCode :
1812132
Title :
Dynamic Performance Analysis of a Certain Solid Rocket Motor Flexibility Nozzle
Author :
Wenzhi, Liu ; Weiliang, Tian ; Jianxin, Wu ; Xiaoqin, Li
Author_Institution :
Mech. Coll., Inner Mongolia Univ. of Technol., Hohhot, China
fYear :
2010
fDate :
24-25 July 2010
Firstpage :
386
Lastpage :
389
Abstract :
The decision of a particular model of solid rocket motor nozzle control precision and flexible functioning of the pivot center drift and systems for power moment problems, using computer-aided design and analysis methods, and establish flexible nozzle coupled rigid-flexible multi-body dynamic model; to role of the body in the system activity for work on the axial load resistance, for sine wave, rectangular wave and triangular wave dynamics under the three kinds of incentive calculation, obtained and analyzed the system for dynamic moments, pivot center drift, supporting ear at a total displacement of, Coulomb friction torque, torque and inertia moment of deviation, while laying the foundation for the system optimization.
Keywords :
CAD; mechanical engineering computing; nozzles; rockets; shear modulus; torque; Coulomb friction torque; axial load resistance; computer aided design; dynamic performance analysis; incentive calculation; inertia moment; nozzle control precision; rigid flexible multibody dynamic model; solid rocket motor; system optimization; Actuators; Analytical models; Angular velocity; Equations; Joints; Mathematical model; Torque; driving moment; dynamic performance; flexible nozzle; pivot center drift; solid propellant rocket motor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information Technology and Computer Science (ITCS), 2010 Second International Conference on
Conference_Location :
Kiev
Print_ISBN :
978-1-4244-7293-2
Electronic_ISBN :
978-1-4244-7294-9
Type :
conf
DOI :
10.1109/ITCS.2010.100
Filename :
5557347
Link To Document :
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