[1]王 刚,刘钧圣,王 琨,等.一种亚声速导弹气动力计算方法[J].弹箭与制导学报,2018,38(02):65-68,73.[doi:10.15892/j.cnki.djzdxb.2018.02.015]
 WANG Gang,LIU Junsheng,WANG Kun,et al.A Method to Predict Aerodynamic Characteristics for Subsonic Missile[J].,2018,38(02):65-68,73.[doi:10.15892/j.cnki.djzdxb.2018.02.015]
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一种亚声速导弹气动力计算方法

参考文献/References:

[1] BLAKE W B. Missile DATCOM user's manual-1997 Fortran 90 version: AFRL-VA-WP-TR-1998-3009 [R]. Ohio: Wright-Patterson Air Force Research Laboratory, 1998.
[2] MOORE F G, MCLNVILLE R M, HYMER T C. The 1998 Version of the NSWC aeroprediction code, Part I:summary of new theoretical methodology: NSWCDD/TR-98/1 [R]. Dahlgren: Naval Surface Warfare Center Dahlgren Division,
1998.
[3] ATTA E H. Numerical simulation of missiles flow fields: AIAA-92-4353-CP [R]. Reston: AIAA, 1992.
[4] 张瑞民, 时晓天. 有翼导弹动态气动特性数值研究 [J]. 弹箭与制导学报, 2017, 37(1): 117-120.
[5] MELIN T. A vortex lattice MATLAB implementation for linear aerodynamic wing applications [D]. Stockholm: Royal Institute of Technology, 2000.
[6] 徐敏, 安效民. 飞行器空气动力特性分析与计算方法 [M]. 西安: 西北工业大学出版社, 2012: 97-106.
[7] 张锡金. 飞行设计手册: 气动设计 [M]. 北京: 航空工业出版社, 2002: 269-270.
[8] 米百刚, 詹浩, 朱军. 基于CFD数值仿真技术的飞行器动导数计算 [J]. 空气动力学报, 2014, 32(6): 834-
839.
[9] RONCH A D, VALLESPIN D, GHOREYSHI M, et al. Evaluation of dynamic derivatives using computational fluid dynamics [J]. AIAA Journal, 2012, 50(2): 470-484.
[10] TAIRA K, ROWLEY C W, COLONIUS T, et al. Lift enhancement for low-aspect-ratio wings with periodic excitation [J]. AIAA Journal, 2010, 48(8): 1785-1790.

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备注/Memo

收稿日期:2017-10-21 第一作者简介:王刚(1988-),男,陕西宝鸡人,工程师,博士,研究方向:战术导弹总体设计。

更新日期/Last Update:

2018-02-11