Title :
Notice of Retraction
Numerical Simulation on Flow Fields of the Blockerless Thrust Reverser
Author :
Yun-Hao Zhang ; Eriqitai ; Xiao-Xing Li
Author_Institution :
Sch. of Mech. Eng. & Autom., Beihang Univ., 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.
The flow fields of a blockerless thrust reverser model were studied using computational fluid dynamic (CFD). The numerical simulations were performed with the bypass ratio of 9. The effects of cascade flow ratio and the injection flow ratio with variation of injection parameters at different fan nozzle pressure ratio (FNPR) were studied. According to detailed analysis of the thrust reverser flow characteristics, that the location of secondary injection, slot angle, injection pressure ratio and slot width on the performance of thrust reversers have a great impact. By the investigation, the optimum value of injection parameter can be found.
Keywords :
computational fluid dynamics; fans; flow simulation; nozzles; numerical analysis; CFD; FNPR; blockerless thrust reverser; cascade flow; computational fluid dynamic; fan nozzle pressure ratio; flow fields; flow simulation; injection flow ratio; numerical simulation; thrust reverser flow; Atmospheric modeling; Computational fluid dynamics; Computational modeling; Ducts; Engines; Mathematical model; Numerical models;
Conference_Titel :
Circuits, Communications and System (PACCS), 2011 Third Pacific-Asia Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4577-0855-8
DOI :
10.1109/PACCS.2011.5990277
