Title :
Notice of Retraction
Optimization design of the rocket launching facilities and the thermal protection
Author :
Jiang Yi ; Ma Yan-li ; Wang Wei-chen ; Hao Ji-guang
Author_Institution :
Dept. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
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.
Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.
Keywords :
aerospace instrumentation; computational fluid dynamics; rockets; computational fluid dynamics method; double-faced deflector; fully hexahedral mesh; k-e turbulence model; optimization design; pressure parameters; rocket launching facilities; temperature parameters; thermal protection; Computational modeling; Design optimization; Equations; Kinetic energy; Numerical simulation; Protection; Rockets; Temperature sensors; Thermal engineering; Thermal stresses; deflector; launching facilities; numerical simulation; rocket plume; thermal protection;
Conference_Titel :
Advanced Computer Control (ICACC), 2010 2nd International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4244-5845-5
DOI :
10.1109/ICACC.2010.5487017
