DocumentCode
533034
Title
Notice of Retraction
Numerical simulation of the initial disturbance influencing on intensive degree
Author
Li Chuanda
Author_Institution
Coll. of Inf. & Commun. Eng., North Univ. of China, Taiyuan, China
Volume
13
fYear
2010
fDate
22-24 Oct. 2010
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
With regard to the research object of a kind of rocket projectile, the influence of gun muzzle vibration by jet impact is considered. Both the launching dynamic model and the intensive degree model are founded. The circumstances of firing time partition for 0.3s to 0.5s are simulated numerically. The results are compared, and the way to improve the intensive degree is presented as well.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
With regard to the research object of a kind of rocket projectile, the influence of gun muzzle vibration by jet impact is considered. Both the launching dynamic model and the intensive degree model are founded. The circumstances of firing time partition for 0.3s to 0.5s are simulated numerically. The results are compared, and the way to improve the intensive degree is presented as well.
Keywords
ballistics; impact (mechanical); numerical analysis; projectiles; rockets; vibrations; weapons; firing time partition; gun muzzle vibration; jet impact; launching dynamic model; rocket projectiles; time 0.3 s to 0.5 s; Aerodynamics; Dispersion; Firing; Force; Mathematical model; Projectiles; Rockets; exterior ballistic trajectories; initial disturbance; intensive degree; rocket projectile;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location
Taiyuan
Print_ISBN
978-1-4244-7235-2
Type
conf
DOI
10.1109/ICCASM.2010.5622715
Filename
5622715
Link To Document