| [1]陈志会, 宁雷, 王鹏.运载火箭助推器回收技术分析与启示[J].宇航总体技术, 2021, 5(05):66-74[2]STEPHEN C.回收火箭迈出关键一步[J].求知导刊, 2014, 4(12):34-37[3]王辰, 张宏剑, 闫伟, 等.重复使用运载火箭栅格舵选型设计与工艺方案研究[J].深空探测学报中英文, 2021, 8(01):51-61[4]HUGHSON M, BLADES E, ABATE G.Transonic aerodynamic analysis of lattice grid tail fin missiles[J].24th AIAA Applied Aerodynamics Conference, 2006, 1(1):3651-3651[5]SZIROCZAK D, SMITH H.A review of design issues specific to hypersonic flight vehicles[J].Progress in Aerospace Sciences, 2016, 84(1):1-28[6]BROOKS R A, BURKHALTER J E.Experimental and analytical analysis of grid fin configurations[J].Journal of Aircraft, 1989, 26(9):885-887[7]WASHINGTON W, MILLER M.Grid fins: a new concept for missile stability and control[C]//31st Aerospace Sciences Meeting. Reno: AIAA, 1993: 35.[8]MILLER M, WASHINGTON W.An experimental investigation of grid fin drag reduction techniques[C]//12th Applied Aerodynamics Conference. Colorado Springs: AIAA, 1994: 1914.[9]GUYOT D, SCHüLEIN E.Novel Locally Swept Lattice Wings for Missile Control at High Speeds[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2007: 63.[10]ABATE G, DUCKERSCHEIN R, HATHAWAY W.Subsonic/transonic free-flight tests of a generic missile with grid fins[C]//38th Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2000: 937.[11]ABATE G, WINCHENBACH G, HATHAWAY W.Transonic aerodynamic and scaling issues for lattice fin projectiles tested in a ballistics range[C]//19th International Symposium of Ballistics. Thun, Switzerland: IBS 2001 Symposium Office, 2001: 413-420.[12]雷娟棉, 吴小胜, 吴甲生.格栅尾翼舵外形参数对气动特性的影响[J].北京理工大学学报, 2007, 08(1):675-679[13]CHEN S, KHALID M, XU H, et al.A comprehensive CFD investigation of grid fins as efficient control surface devices[C]//38th Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2000: 987.[14]THEERTHAMALAI P, BALAKRISHNAN N.Effect of geometric parameters on the aerodynamic characteristics of grid-fin cells at supersonic speeds[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2007: 690.[15]杜涛, 许晨舟, 王国辉, 等.人工智能气动特性预测技术在火箭子级落区控制项目的应用[J].宇航学报, 2021, 42(01):61-73[16]杜涛, 龚安龙, 唐伟, 等.局部后掠型栅格舵的气动特性研究[J].宇航总体技术, 2021, 5(02):14-23[17]李永红, 黄勇, 陈建中, 等.曲面形栅格翼气动特性研究[J].空气动力学学报, 2016, 34(4):536-540[18]李永红, 杨晓娟, 陈建中, 等.超声速栅格舵弹身干扰特性数值模拟与试验研究[J].北京航空航天大学学报, 2021, 47(05):953-960[19]张培红, 贾洪印, 郭勇颜, 等.基于软件的栅格舵气动特性模拟[J].计算力学学报, 2021, 39(4):1-9[20]周铸, 黄江涛, 黄勇, 等.技术在航空工程领域的应用、挑战与发展[J].航空学报, 2017, 38(3):20891-020891[21]韩忠华.模型及代理优化算法研究新进展[J].航空学报, 2016, 37(11):3197-3225[22]乔建领, 韩忠华, 宋文萍.基于代理模型的高效全局低音爆优化设计方法[J].航空学报, 2018, 39(05):67-80[23]LIU F, HAN Z H, ZHANG Y, et al.Surrogate-based aerodynamic shape optimization of hypersonic flows considering transonic performance[J].Aerospace Science and Technology, 2019, 93(1):105345-105345[24]张阳, 韩忠华, 柳斐, 等.高超声速飞行器宽速域翼型高效多目标优化设计方法研究[J].航空科学技术, 2020, 31(11):14-24[25]李永红.栅格翼气动特性数值模拟与外形参数优化研究[D]. 绵阳: 中国空气动力研究与发展中心, 2012: 25-51.[26]PENG K, HU F, WANG D, et al.Grid fins shape design of a launch vehicle based on sequential approximation optimization[J].Advances in Space Research, 2018, 62(7):1863-1878[27]LEDLOW T W, BURKHALTER J E, Hartfield R J.Integration of grid fins for the optimal design of missile systems[C]//AIAA Atmospheric Flight Mechanics Conference. Kissimmee: AIAA, 2015: 1017.[28]ORTHNER K S.Aerodynamic analysis of lattice grids in transonic flow[D]. Ohio, Air Force Institute of Technology, Dept of Aeronautics and Astronautics, 2004.[29]ZENG Y, CAI J S, DEBIASI M, et al.Numerical study on drag reduction for grid-fin configurations[C]//47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando: AIAA, 2009: 1105.[30]MCKAY M D, BECKMAN R J, CONOVER W J, et al.A comparison of three methods for selecting values of input variables in the analysis of output from a computer code[J].Technometrics, 2000, 42(1):55-61[31]HAN Z H.SurroOpt: A generic surrogate-based optimization code for aerodynamic and multidisciplinary design[C]//30th Congress of the International Council of the Aeronautical Sciences. Daejeon: ICAS, 2016. |
CJA
