DocumentCode :
2089028
Title :
An Interior Ballistic Simulation of the Gas-steam Missile Ejection
Author :
Yongquan Liu ; Anmin Xi ; Hongfei Liu
Author_Institution :
Sch. of Mech. Eng., Univ. of Sci. & Technol. Beijing, Beijing, China
Volume :
4
fYear :
2010
fDate :
14-15 Aug. 2010
Firstpage :
235
Lastpage :
237
Abstract :
An interior ballistic simulation of the canister launched missiles has been developed with the help of FLUENT. One of the special features of this simulation is the almost uniform acceleration which occurs 0.25s after startup and keeps the missile shockless during ejection. The calculation was done efficiently in FLUENT after setting all the required parameters. Several figures have been given to show the velocity and pressure of the flow field in the reservoir. The variations of the velocity and acceleration with time show that the simulation and the test data of the experiments are in good agreement with each other. This model can be used to analyze the similar launch procedures.
Keywords :
ballistics; missiles; FLUENT; acceleration; canister launched missiles; flow field; gas-steam missile ejection; interior ballistic simulation; reservoir; velocity; Acceleration; Analytical models; Equations; Generators; Mathematical model; Missiles; Reservoirs; gas-steam ejection; interior ballistic simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information Engineering (ICIE), 2010 WASE International Conference on
Conference_Location :
Beidaihe, Hebei
Print_ISBN :
978-1-4244-7506-3
Electronic_ISBN :
978-1-4244-7507-0
Type :
conf
DOI :
10.1109/ICIE.2010.346
Filename :
5572728
Link To Document :
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