[1]那旭东,夏智勋,马立坤,等.先进火箭仿真中心Rocstar程序概述[J].固体火箭技术,2019,42(01):7-15.
 NA Xudong,XIA Zhixun,MA Likun,et al.Introduction of Rocstar codes developed by the centerfor simulation of advanced rockets[J].Journal of Solid Rocket Technology,2019,42(01):7-15.
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先进火箭仿真中心Rocstar程序概述

参考文献/References:

[1]武晓松,陈军,王栋,等. 固体火箭发动机工作过程数值仿真[M].北京:高等教育出版社,2006.WU Xiaosong,CHEN Jun,WANG Dong,et al.Numerical simulation of operation process of solid rocket motor [M].Higher Education Press,2006.

[2]Dick W,Fiedler R,Heath M.Building rocstar: simulation science for solid propellant rocket motors [C]//In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Sacramento,California,9-12 July 2006.
[3]Haselbacher A,Najjar F,Massa L,et al.Enabling three-dimensional unsteady SRM burn-out computations by slow-time acceleration[C]//In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Sacramento,California,9-12 July 2006.
[4]Dick W,Heath M,Fiedler R,et al.Advanced simulation of solid propellant rockets from first principles[C]//In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Tucson,Arizona,10-13 July 2005.
[5]唐金兰,刘佩进.固体火箭发动机原理[M].北京:国防工业出版社,2013.TANG Jinlan,LIU Peijin.Principle of solid rocket motor [M].National Defense Industry Press,2013.
[6]Dauch F,Ribereau D.A software for SRM grain design and internal ballistics evaluation,PIBAL[C]//In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Indianapolis,Indiana,7-10 July 2002.
[7]解红雨,张为华,王锦荷,等.固体火箭发动机虚拟样机集成设计环境[J].固体火箭技术,2006,29(1):15-18+51.XIE Hongyu,ZHANG Weihua,WANG Yinhe,et al.Integrated design environment for virtual prototyping of solid rocket motor[J].Journal of Solid Rocket Technology,2006,29(1):15-18+51.[8]蔡强,鲍福廷.基于ACIS几何造型平台的固体火箭发动机装药设计[J].固体火箭技术,2008,31(3):236-238+242.CAI Qiang,BAO Futing.Grain design of solid rocket motor based on ACIS geometric modelling platform[J].Journal of Solid Rocket Technology,2008,31(3):236-238+242.
[9]冯喜平,董韬,李进贤,等.固体火箭发动机地面试验测量系统研究[J].固体火箭技术,2009,32(6):702-705.FENG Xiping,DONG Tao,LI Jinxian,et al.Research on measurement and control system for solid rocket motor tests[J].Journal of Solid Rocket Technology,2009,32(6):702-705.
[10]CAVALLINI E.Modeling and numerical simulation of solid rocket motors internal ballistics[D].Sapienza Università,2010.
[11]魏瀚,鲍福廷,蔡强,等.固体火箭发动机参数辨识软件关键技术研究[J].科学技术与工程,2011,11(36):9016-9020.WEI Han,BAO Futing,CAI Qiang,et al.Research on enabling techniques for identification software for solid rocket motor model parameters[J].Science Technology and Engineering,2011,11(36):9016-9020.
[12]Gueyffier D,Roux F X,Fabignon Y,et al.Accurate computation of grain burning coupled with flow simulation in rocket chamber [J].Journal of Propulsion and Power,2015,31(6): 1761-1776.
[13]Brandyberry M,Campbell M,Wasistho B,et al.Rocstar simulation suite: An advanced 3-D multiphysics,multiscale computational framework for tightly coupled,fluid-structure-thermal applications[C]//In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Atlanta,Georgia,30 July-01 August 2012.
[14]高双武,强洪夫,周伟,等.基于子循环预测校正的三维SRM点火瞬态流固耦合数值模拟[J].计算力学学报,2011,28(S1):84-89.GAO Shuangwu,QIANG Hongfu,ZHOU Wei,et al.Fluid-structure interaction numerical simulation of 3D SRM during ignition with subcycling based predict-correct scheme [J].Chinese Journal of Computational Mechanics,2011,28(S1):84-89.
[15]李猛,王宏.火箭发动机排气羽流特征信号预示技术研究综述 [J].飞航导弹,2010(3):54-57+60.LI Meng,WANG Hong.Overview of rocket engine exhaust plume characteristic signal prediction technology [J].Aerodynamic Missile Journal,2010(3):54-57+60.
[16]CSAR.Center for simulation of advanced rockets 2004 annual report [R].2004.
[17]CSAR.Center for simulation of advanced rockets 2003 annual report[R].2003.
[18]CSAR.Center for simulation of advanced rockets 1997-98 annual report[R].1998.[19]CSAR.Rocstar simulation codes [CP/OL].http://www.csar.illinois.edu/,2004.?
[20]Heath M,Dick W.Virtual prototyping of solid propellant rockets [J].Computing in Science & Engineering.2000,2(2): 21-32.
[21]Illinois Rocstar LLC.Rocstar simulation suite[CP/OL].http://www.illinoisrocstar.com/products/rocstar,2018.
[22]CSAR.Center for Simulation of Advanced Rockets 2006 Annual Report [R].2006.
[23]Dick W,Heath M,Fiedler R.Integrated 3-D simulation of solid propellant rockets[C]//In 37th Joint Propulsion Conference and Exhibit.Salt Lake City,Utah,USA,9-11 July 2001.
[24]Illinois Rocstar LLC.Rocstar multiphysics application [CP/OL].https://sourceforge.net/projects/rocstar/,November 2015.
[25]Illinois Rocstar LLC.Rocstar multiphysics simulation application[CP/OL].https://github.com/IllinoisRocstar/Rocstar,March 2013.
[26]Jiao X.Face offsetting: A unified approach for explicit moving interfaces[J].J.Comput.Phys.,2007,220(2): 612-625.
[27]Freitag L,Leurent T,Knupp P,et al.MESQUITE design:issues in the evelopment of a mesh quality improvement toolkit [R].2002.
[28]Fiedler R,Jiao X,Namazifard A,et al.Coupled fluid-structure 3-D solid rocket motor simulations [C]//In 37th Joint Propulsion Conference and Exhibit.AIAA 2001-3954.
[29]Illinois Rocstar LLC.Rocketeer users guide version 1.3.6 [M].Illinois: Illinois Rocstar LLC,2014.
[30]徐学文,牟俊林,彭军.固体火箭发动机的三维仿真研究动态[J].航空计算机技术,2007,37(3):100-103.XU Xuewen,MU Junlin,PENG Jun.Research trend in three-dimension simulation for the solid rocket motor [J].Aeronautical Computing Technique,2007,37(3):100-103.
[31]Fiedler R,Breitenfeld M,Jiao X,et al.Simulations of slumping propellant and flexing inhibitors in solid rocket motors[C]//In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Indianapolis,Indiana,7-10 July 2002.
[32]Brandyberry M,Fiedler R,McLay C.Verification and validation of the Rocstar 3-D multi-physics solid rocket motor simulation program[C]//In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Tucson,Arizona,10-13 July 2005.
[33]Park C,Haftka R T,Kim N H.Validation,uncertainty quantification and uncertainty reduction for a shock tube simulation[C]//In 18th AIAA Non-Deterministic Approaches Conference.San Diego,California,USA,4-8 January 2016.
[34]Fiedler R,Namazifard A,Campbell M,et al.Detailed simulations of propellant slumping in the Titan-IV SRMU PQM-1[C]//In 42nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit.Sacramento,California,9-12 July 2006.
[35]曹琪,李晓娜,李进贤,等.固体火箭发动机点火瞬间流固耦合综述 [J].中国科学:技术科学,2011,41(6):703-709.CAO Qi,LI Xiaona,LI Jinxian,et al.Overview of fluidsolid interaction of ignition transients in solid rocket motor [J].Scientia Sinica Technologica,2011,41(6):703-709.
[36]周红梅,于胜春,王宏伟,等.固体火箭发动机点火过程流固耦合仿真研究综述[J].飞航导弹,2008(7):54-57.ZHOU Hongmei,YU Shengcun,WANG Hongwei,et al.Review of fluid-solid coupling simulation for solid rocket motor ignition process[J].Aerodynamic Missile Journal,2008(7):54-57.
[37]Illinois Rocstar LLC.Rocstar tutorial: Section 9 data set creation[M].Illinois Rocstar LLC,2012.

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更新日期/Last Update: 2019-03-21
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