ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2022, Vol. 43 ›› Issue (9): 25950-025950.doi: 10.7527/S1000-6893.2021.25950
• Reviews • Previous Articles Next Articles
SONG Wei, AI Bangcheng
Received:
2021-06-10
Revised:
2021-08-03
Online:
2022-09-15
Published:
2021-08-17
CLC Number:
SONG Wei, AI Bangcheng. Multibody separation dynamics: Review[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 25950-025950.
[1] FEDOROV A V, SOUDAKOV V G, MALMUTH N D. Theoretical modeling of two-body interaction in supersonic flow[J]. AIAA Journal, 2010, 48(2): 258-266. [2] WANG G, CHEN X, XING Y, et al. Multi-body separation simulation with an improved general mesh deformation method[J]. Aerospace Science and Technology, 2017, 71: 763-771. [3] PERILLO S, ATKINS D, ROBERTS W. Challenges and emerging trends in store separation engineering: an air force SEEK EAGLE office perspective[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. [4] HAYWARD D M, DUFF A, WAGNER C. F-35 weapons design integration[C]//2018 Aviation Technology, Integration, and Operations Conference. Reston: AIAA, 2018. [5] CHARLTON E, DAVIS M. Computational optimization of the F-35 external fuel tank for store separation[C]//46th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2008. [6] ROCK S, HABCHI S, LINGARD J, et al. Computational investigation of wind tunnel support interference for an ejection seat test[C]//17th Applied Aerodynamics Conference. Reston: AIAA, 1999. [7] MURPHY K, BUNING P, PAMADI B, et al. Overview of transonic to hypersonic stage separation tool development for multi-stage-to-orbit concepts[C]//24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2004. [8] BERMUDEZ L, GLADDEN R. Aerodynamic characterization of the hyper-X launch vehicle (HXLV)[C]//12th AIAA International Space Planes and Hypersonic Systems and Technologies. Reston: AIAA, 2003. [9] DISSEL A F, KOTHARI A P, LEWIS M J. Investigation of two-stage-to-orbit airbreathing launch-vehicle configurations[J]. Journal of Spacecraft and Rockets, 2006, 43(3): 568-574. [10] BAI Z N, CAI W J, ZHOU J J, et al. Research on multi-body aerodynamic interference during torpedo-rocket separation[J]. Acta Armamentarii, 2017, 38(11): 2176-2183 (in Chinese). 白治宁, 蔡卫军, 周景军, 等. 助飞鱼雷雷箭分离多体气动干扰特性研究[J]. 兵工学报, 2017, 38(11): 2176-2183. [11] DAGAN Y, ARAD E. Analysis of shroud release applied for high-velocity missiles[J]. Journal of Spacecraft and Rockets, 2013, 51(1): 57-65. [12] WANG J L, WANG H, TAO R Y, et al. The movement characteristics analysis of interference flow field on the separation of multi-bay cluster munition[J]. Acta Aerodynamica Sinica, 2016, 34(4): 490-496 (in Chinese). 王金龙, 王浩, 陶如意, 等. 子母弹不同舱段分离流场特性及运动特性研究[J]. 空气动力学学报, 2016, 34(4): 490-496. [13] SONG W, Ai B C. Research progress on multibody aerodynamics[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(6): 1461-1484 (in Chinese). 宋威, 艾邦成. 多体空气动力学研究进展[J]. 力学学报, 2022, 54(6): 1461-1484. [14] JAMISON K A. Grid-mode transonic store separation analyses using modern design of experiments[C]//31 st Congress of the International Council of the Aeronautical Science, 2018. [15] LOUPY G J M, BARAKOS G N, TAYLOR N J. Store release trajectory variability from weapon bays using scale-adaptive simulations[J]. AIAA Journal, 2017, 56(2): 752-764. [16] MOELYADI M A, BREITSAMTER C, LASCHKA B. Stage-separation aerodynamics of two-stage space transport systems Part1: steady-state simulations[J]. Journal of Spacecraft and Rockets, 2008, 45(6): 1230-1239. [17] LIEVER P, HABCHI S, ENGELUND W, et al. Stage separation analysis of the X-43A research vehicle[C]//22nd Applied Aerodynamics Conference and Exhibit. Reston: AIAA, 2004. [18] LIU Y, QIAN Z S, LU W B, et al. Numerical investigation on the safe stage-separation mode for a TSTO vehicle[J]. Aerospace Science and Technology, 2020, 107: 106349. [19] RESCH L, ZENTZ L, ALLWINE J. Hypersonic shroud separation testing and modelling capabilities at the naval surface warfare center hypervelocity wind tunnel 9[C]//25th Plasmadynamics and Lasers Conference. Reston: AIAA, 1994. [20] CHEN S T, YU Y. Numerical simulation of attitude motion of submunition during dispensing in supersonic flow field[J]. Journal of Ballistics, 2019, 31(1): 29-35 (in Chinese). 陈时通, 于勇. 超声速流场中子母弹分离与子弹姿态变化规律的数值模拟[J]. 弹道学报, 2019, 31(1): 29-35. [21] EDGE H, SAHU J, HEAVEY K. Computational fluid dynamics modeling of submunition separation from missile[C]//17th Applied Aerodynamics Conference. Reston: AIAA, 1999. [22] LASEK M, SIBILSKI K. Modelling of external store separation[C]//40th AIAA Aerospace Sciences Meeting & Exhibit. Reston: AIAA, 2002. [23] TARTABINI P V, ROITHMAYR C M, TONIOLO M D, et al. Modeling multibody stage separation dynamics using constraint force equation methodology[J]. Journal of Spacecraft and Rockets, 2011, 48(4): 573-583. [24] CARTER R, LIND R. Trajectory optimization for guided store separation[C]//AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2012. [25] XU M, AN X M. Analysis and calculation method of aerodynamic characteristics of aircraft[M]. Xi'an: Northwestern Polytechnical University Press, 2012 (in Chinese). 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. [26] MALMUTH N D. Theoretical aerodynamics in today's real world: opportunities and challenges[J]. AIAA Journal, 2006, 44(7): 1377-1392. [27] VAN DEN BROEK G J. The use of a panel method in the prediction of external store separation[J]. Journal of Aircraft, 1984, 21(5): 309-315. [28] KAYKAYOGLU C. Application of the vortex lattice CFD method to obtaining unsteady aerodynamic predictions about wing/fuselage/pylon/store configuration including store separation[C]//34th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1996. [29] CENKO A, CRAIG K, TSENG W, et al. IFM applications to theoretical trajectory predictions[C]//25th AIAA Aerospace Sciences Meeting. Reston: AIAA, 1987. [30] DILLENIUS M, GOODWIN F, NIELSEN J. Extension of the method for predicting six-degree-of-freedom store separation trajectories at speeds up to the critical speed to include a fuselage with noncircular cross section. volume I-Theoretical methods and comparisons with experiment: AFFDL-TR-74-130[R]. Washington, D.C. : NASA, 1974. [31] DESLANDES R. Evaluation of aircraft interference effects on external stores at subsonic and transonic speeds: AGARD-CP-285-6[R]. Paris: AGARD, 1980. [32] CROSS A G T. Calculation of three-dimentional viscous flow involving regions of strong interaction[C]//British Aerospace, 1988. [33] ISAACS D. The prediction of carriage loads and changes in aircraft longitudinal stability for pylon-mounted stores at subsonic speed[C]//RAE Store, Carriage, and Release conference, Royal Aeronautical Society, 1990. [34] HALLBERG E, GODIKSEN W. MATLAB based telemetry integration utility for store separation analysis: AIAA-2007-1643[R]. Reston: AIAA, 2007. [35] PAMADI B N, TARTABINI P V, TONIOLO M D, et al. Application of constraint force equation methodology for launch vehicle stage separation[J]. Journal of Spacecraft and Rockets, 2013, 50(1): 191-205. [36] WANG J N, LIU L, BU K C. Kinetic analysis and simulation of stage separation for hypersonic velocity kinetic energy missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2003, 23(S6): 50-52 (in Chinese). 王竞男, 刘莉, 卜奎晨. 高速动能导弹级间分离动力学分析与仿真[J]. 弹箭与制导学报, 2003, 23(S6): 50-52. [37] WANG X, YUAN X G, YANG X. Research on multi-body separation dynamics using Lagrange method[J]. Journal of Northwestern Polytechnical University, 2014, 32(1): 18-22 (in Chinese). 王鑫, 袁晓光, 杨星. 基于拉格朗日方法的飞行器多体分离姿态动力学分析研究[J]. 西北工业大学学报, 2014, 32(1): 18-22. [38] WANG J N, LIU L. Dynamic simulation of stage separation of missile based on ADAMS[J]. Journal of System Simulation, 2006, 18(12): 3512-3514, 3519 (in Chinese). 王竞男, 刘莉. 基于ADAMS的导弹级间分离动力学仿真[J]. 系统仿真学报, 2006, 18(12): 3512-3514, 3519. [39] PAMADI B N, TARTABINI P V, TONIOLO M D, et al. Application of CFE/POST2 for simulation of launch vehicle stage separation: AIAA-2009-5842[R]. Reston: AIAA, 2009. [40] DAVIDS S, CENKO A. Grid based approach to store separation[C]//19th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2001. [41] BAMBER M. Store separation investigations by grid method using wind tunnel data[R]. 2010. [42] HEMSCH M J. Tactical missile aerodynamics: general topics[M]. Reston: AIAA, 1992. [43] CHING T K. Grid survey approach to store separation trajectory prediction[J]. Journal of Aircraft, 2000, 37(4): 736-738. [44] MOYER S A, TALBOT M D. Wind-tunnel test techniques for unmanned aerial vehicle separation investigations[J]. Journal of Aircraft, 1994, 31(3): 585-590. [45] BOWER W, KIBENS V, CARY A, et al. High-frequency excitation active flow control for high-speed weapon release (HIFEX)[C]//2nd AIAA Flow Control Conference. Reston: AIAA, 2004. [46] BORDELON W, FROST A, REED D. Stage separation wind tunnel tests of a generic TSTO launch vehicle[C]//21st AIAA Applied Aerodynamics Conference. Reston: AIAA, 2003. [47] TAO R Y, WANG F H, JI X S, et al. Aerodynamic interference wind tunnel experiment for separation of supersonic cluster munition[J]. Journal of Ballistics, 2008, 20(4): 24-27 (in Chinese). 陶如意, 王福华, 季晓松, 等. 超音速子母弹分离气动干扰风洞试验[J]. 弹道学报, 2008, 20(4): 24-27. [48] LEE J, DUNWORTH K, RIZK M, et al. Studies of combined use of CFD and wind tunnel test approaches to simulate a store separation from F-15E using efficient CFD database generation[C]//22nd Applied Aerodynamics Conference and Exhibit. Reston: AIAA, 2004. [49] MORGRET C, SMITH M, MOORE D. FLIP 4 store-separation trajectory simulation code[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. [50] SONG W, AI B C, JIANG Z H, et al. Prediction and assessment of drop separation compatibility of internal weapons by wind tunnel drop-test[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 523415 (in Chinese). 宋威, 艾邦成, 蒋增辉, 等. 内埋武器投放分离相容性的风洞投放试验预测与评估[J]. 航空学报, 2020, 41(6): 523415. [51] FLORA T J. Freedrop testing and CFD simulation of ice models from a cavity into supersonic flow[D]. Washington, D.C. : Air Force Institute of Technology, 2012. [52] JIANG Z H, SONG W, JIA Q Y, et al. Wind tunnel free-flight test for multi-bodies separation[J]. Acta Aerodynamica Sinica, 2016, 34(5): 581-586 (in Chinese). 蒋增辉, 宋威, 贾区耀, 等. 多体分离风洞自由飞试验[J]. 空气动力学学报, 2016, 34(5): 581-586. [53] YANG C X, HAN H Y, GONG J, et al. Prediction of the aircraft canopy trajectory[J]. Acta Aerodynamica Sinica, 2005, 23(1): 35-39 (in Chinese). 杨春信, 韩海鹰, 龚洁, 等. 弹射过程座舱盖抛放轨迹的预测[J]. 空气动力学学报, 2005, 23(1): 35-39. [54] XIA J, TIAN S L, WANG J F, et al. Parallel computing strategy for 3D dynamic overset unstructured navier-stokes solver[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(5): 1118-1124 (in Chinese). 夏健, 田书玲, 王江峰, 等. 三维动态非结构重叠网格Navier-Stokes方程并行算法[J]. 航空学报, 2008, 29(5): 1118-1124. [55] MADSON M, MOYER S, CENKO A. TranAir computations of the flow about a generic wing/pylon/finned-store configuration[C]//32nd Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1994. [56] HARISH G, PAVANAKUMAR M, ANANDHANAR-AYANAN K. Store separation dynamics using grid-free Euler solver[C]//24th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2006. [57] LIJEWSKI L E, SUHS N E. Time-accurate computational fluid dynamics approach to transonic store separation trajectory prediction[J]. Journal of Aircraft, 1994, 31(4): 886-891. [58] PREWITT N C, BELK D M, MAPLE R C. Multiple-body trajectory calculations using the beggar code[J]. Journal of Aircraft, 1999, 36(5): 802-808. [59] BENMEDDOUR A, FORTIN F, AMIRLATIFI T, et al. Prediction of the CF-18/MK-83 LD store separation characteristics using a quasi-steady CFD approach[C]//21 st AIAA Applied Aerodynamics Conference. Reston: AIAA, 2003. [60] XU X P, ZHOU Z, FAN R J, et al. Research on release of airborne weapon based on dynamic chimera grid technique[J]. Acta Armamentarii, 2010, 31(9): 1241-1246 (in Chinese). 许晓平, 周洲, 范锐军, 等. 基于动态嵌套网格技术的机载武器投放研究[J]. 兵工学报, 2010, 31(9): 1241-1246. [61] KIM E, KWON J H, PARK S H. Prediction of ballistic separation effect by direct calculation of incremental coefficients[J]. Journal of Aircraft, 2010, 47(2): 630-637. [62] ARORA K, SHAH V, ANANDHANARAYANAN K, et al. Influence of aircraft flow field on the longitudinal stability of a missile[J]. Defence Science Journal, 2013, 63(3): 242-248. [63] ANANDHANARAYANAN K, ARORA K, SHAH V, et al. Separation dynamics of air-to-air missile using a grid-free Euler solver[J]. Journal of Aircraft, 2013, 50(3): 725-731. [64] CHAKRABORTY D, ANANDHANARAYANAN K, RAJ A, et al. Separation dynamics of air-to-air missile and validation with flight data[J]. Defence Science Journal, 2017, 68(1): 5. [65] BERGLIND T, TYSELL L. Numerical investigation of the impact of maneuver on store separation trajectories[C]//28th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2010. [66] GODIKSEN W H. Effect of targeting pod addition on F-18C store separation characteristics: AIAA-2008-6380[R]. Reston: AIAA, 2008. [67] BAUM J, LUO H, LOEHNER R, et al. Application of unstructured adaptive moving body methodology to the simulation of fuel tank separation from an F-16 fighter[C]//35th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1997. [68] LI X W, FAN X J. Simulation of the release of store based on the moving chimera grid technique[J]. Acta Aerodynamica Sinica, 2004, 22(1): 114-117 (in Chinese). 李孝伟, 范绪箕. 基于动态嵌套网格的飞行器外挂物投放的数值模拟[J]. 空气动力学学报, 2004, 22(1): 114-117. [69] DEMIR H, ALEMDAROGLU N. Trajectory calculation of a store released from a fighter aircraft[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005. [70] BAUM J, LOEHNER R. Numerical simulation of pilot/seat ejection from an F-16[C]//31 st Aerospace Sciences Meeting. Reston: AIAA, 1993. [71] GUO Z, LI X B, QU Z H, et al. Simulation of flows past multi-body in relative motion with dynamic unstructured method[J]. Acta Aerodynamica Sinica, 2001, 19(3): 310-316 (in Chinese). 郭正, 李晓斌, 瞿章华, 刘君. 用非结构动网格方法模拟有相对运动的多体绕流[J]. 空气动力学学报, 2001, 19(3): 310-316. [72] SNYDER D, KOUTSAVDIS E, ANTTONEN J. Transonic store separation using unstructured CFD with dynamic meshing[C]//33rd AIAA Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2003. [73] TOMARO R F, WITZEMAN F C, STRANG W Z. Simulation of store separation for the F/A-18C using cobalt[J]. Journal of Aircraft, 2000, 37(3): 361-367. [74] MURMAN S, AFTOSMIS M, BERGER M. Simulations of 6-DOF motion with a Cartesian method[C]//41 st Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2003. [75] MURMAN S M, AFTOSMIS M J, BERGER M J. Simulations of store separation from an F/A-18 with a Cartesian method[J]. Journal of Aircraft, 2004, 41(4): 870-878. [76] ZHU B, ZHU X P, ZHOU Z, et al. Simulation of unsteady multi-body flowfield involving relative movement based on unstructured mesh[J]. Acta Aerodynamica Sinica, 2013, 31(2): 181-185 (in Chinese). 朱冰, 祝小平, 周洲, 等. 基于非结构动网格的多体分离数值仿真研究[J]. 空气动力学学报, 2013, 31(2): 181-185. [77] YANG M Z, GUI Y W, LIU G, et al. Numerical simulation of missile separation[J]. Acta Aerodynamica Sinica, 2006, 24(2): 261-264 (in Chinese). 杨明智, 桂业伟, 刘刚, 等. 导弹投放分离的数值模拟[J]. 空气动力学学报, 2006, 24(2): 261-264. [78] FORMAGGIA L, PERAIRE J, MORGAN K. Simulation of a store separation using the finite element method[J]. Applied Mathematical Modelling, 1988, 12(2): 175-181. [79] LEE S, PARK M, CHO K W, et al. New fully automated procedure for the prediction of store trajectory[J]. Journal of Aircraft, 2000, 37(6): 1038-1049. [80] SINGH K P, BAYSAL O. Unstructured method for flows past bodies in general three-dimensional relative motion[J]. AIAA Journal, 2001, 39(2): 219-224. [81] LIU J L. Trajectory analyses of external store separation by using the Euler equations[J]. Journal of Aircraft, 2003, 40(1): 206-208. [82] FENG B M, NIE W S, CHE X K, et al. Effect of fixing angle to separation characteristics of internal store[J]. Acta Aerodynamica Sinica, 2010, 28(6): 672-675 (in Chinese). 冯必鸣, 聂万胜, 车学科, 等. 安装角度对内埋式导弹分离特性的影响[J]. 空气动力学学报, 2010, 28(6): 672-675. [83] LUO X B, BAYSAL O. Computational simulation of hypersonic vehicle separation from its booster[C]//9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 1999. [84] BUNING P, GOMEZ R, SCALLION W. CFD approaches for simulation of wing-body stage separation[C]//22nd Applied Aerodynamics Conference and Exhibit. Reston: AIAA, 2004. [85] CHAMBERLAIN R, BALTAR J. Time-accurate calculation of hypersonic shroud separation[C]//31 st Aerospace Sciences Meeting. Reston: AIAA, 1993. [86] WANG W, LIU J, BAI X Z, et al. DUM research and apply to solve the fairing separating form hypersonic vehicle[J]. Acta Aerodynamica Sinica, 2008, 26(1): 131-135 (in Chinese). 王巍, 刘君, 白晓征, 等. 非结构动网格技术及其在超声速飞行器头罩分离模拟中的应用[J]. 空气动力学学报, 2008, 26(1): 131-135. [87] LIN J M, AN F X, YU D B. Shock effects from the dispenser on the aerodynamic characteristics of submunitions[J]. Acta Armamentarii, 2000, 21(4): 334-337 (in Chinese). 林靖明, 安复兴, 于德滨. 母弹激波对子弹气动特性影响的研究[J]. 兵工学报, 2000, 21(4): 334-337. [88] ZHANG Y D, JI C Q. The numerical simulation of unsteady multi-body separating flows[J]. Acta Aerodynamica Sinica, 2006, 24(1): 1-4 (in Chinese). 张玉东, 纪楚群. 多体分离非定常气动特性数值模拟[J]. 空气动力学学报, 2006, 24(1): 1-4. [89] WANG W, LIU J, GUO Z. Numerical simulation of release the cover form cargo projectile[J]. Acta Aerodynamica Sinica, 2006, 24(3): 285-288 (in Chinese). 王巍, 刘君, 郭正. 子母弹抛壳过程非定常流动的数值模拟[J]. 空气动力学学报, 2006, 24(3): 285-288. [90] CHE J, TANG S, XIE C Q. The initial trajectory numerical simulation of air launched missile[J]. Acta Aerodynamica Sinica, 2006, 24(2): 205-208 (in Chinese). 车竞, 唐硕, 谢长强. 空射导弹发射初始弹道数值仿真[J]. 空气动力学学报, 2006, 24(2): 205-208. [91] LEI J M, NIU J P, WANG S Z, et al. Numerical simulation about the effect of initial separation condition on safety of aerial bomb separated from an aircraft[J]. Acta Armamentarii, 2016, 37(2): 357-366 (in Chinese). 雷娟棉, 牛健平, 王锁柱, 等. 初始分离条件对航弹与载机分离安全性影响的数值模拟研究[J]. 兵工学报, 2016, 37(2): 357-366. [92] DUAN X P, CHANG X H, ZHANG L P. A CFD-and-6DOF-coupled solver for multiple moving object problems based on dynamic hybrid grids[J]. Acta Aerodynamica Sinica, 2011, 29(4): 447-452 (in Chinese). 段旭鹏, 常兴华, 张来平. 基于动态混合网格的多体分离数值模拟方法[J]. 空气动力学学报, 2011, 29(4): 447-452. [93] DI Y C, GAO G, XU J L, et al. Time-accurate simulation of the aircraft external store separation[J]. Applied Mechanics and Materials, 2013, 444-445: 854-859. [94] OLEJNIK A, DZIUBIŃSKISKI A, KISZKOWIAK Ł. Separation safety analysis using CFD simulation and remeshing[J]. Aerospace Science and Technology, 2020, 106: 106190. [95] XI K, YAN C. CFD transonic trajectory predictions of three-store ripple release using chimera method[J]. Applied Mechanics and Materials, 2014, 513-517: 4490-4493. [96] NICHOLS R, TRAMEL R, NICHOLS R, et al. Applications of a highly efficient numerical method for overset-mesh moving body problems[C]//15th Applied Aerodynamics Conference. Reston: AIAA, 1997. [97] WELTERLEN T, LEONE C. Application of viscous, Cartesian CFD to aircraft stores carriage and separation simulation[C]//14th Applied Aerodynamics Conference. Reston: AIAA, 1996. [98] AI B C, SONG W, DONG L, et al. Review of aircraft-store separation compatibility of internal weapons[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 023809 (in Chinese). 艾邦成, 宋威, 董垒, 等. 内埋武器机弹分离相容性研究进展综述[J]. 航空学报, 2020, 41(10): 023809. [99] HAN H Y, YANG C X, YANG X M, et al. Unsteady aerodynamics characteristic study of a jettisoned aircraft canopy[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(6): 675-681 (in Chinese). 韩海鹰, 杨春信, 杨新明, 等. 座舱盖抛放过程中的非定常气动特性研究[J]. 航空学报, 2005, 26(6): 675-681. [100] CHEN D H, WU W H, WANG J J. Numerical simulation research of the fighter ejection escape system[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(5): 778-783 (in Chinese). 陈德华, 吴文华, 王晋军. 战斗机弹射救生系统数值模拟研究[J]. 航空学报, 2006, 27(5): 778-783. [101] BUNING P, WONG T C, DILLEY A, et al. Prediction of Hyper-X stage separation aerodynamics using CFD[C]//18th Applied Aerodynamics Conference. Reston: AIAA, 2000. [102] CAVALLO P, DASH S. Aerodynamics of multi-body separation using adaptive unstructured grids[C]//18th Applied Aerodynamics Conference. Reston: AIAA, 2000. [103] TIAN S L, FU J W, CHEN J T. A numerical method for multi-body separation with collisions[J]. Aerospace Science and Technology, 2021, 109: 106426. [104] WANG Z W, WANG H, RUAN W J, et al. Simulation of plates group initial separation in high speed[J]. Acta Aerodynamica Sinica, 2015, 33(6): 828-834 (in Chinese). 王政伟, 王浩, 阮文俊, 等. 高速下集束薄片初始分离过程仿真研究[J]. 空气动力学学报, 2015, 33(6): 828-834. [105] JORDAN J, DENNY A, JORDAN J, et al. Approximation methods for computational trajectory predictions of a store released from a bay[C]//15th Applied Aerodynamics Conference. Reston: AIAA, 1997. [106] SHIPMAN J, ARUNAJATESAN S, CAVALLO P, et al. Flow control for enhanced store separation[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2007. [107] HANKEY W L, SHANG J S. Analyses of pressure oscillations in an open cavity[J]. AIAA Journal, 1980, 18(8): 892-898. [108] SONG W, LU W, JIANG Z H, et al. The crucial technique investigation of wind-tunnel drop-model testing for the supersonic internal weapons[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(6): 1346-1355 (in Chinese). 宋威, 鲁伟, 蒋增辉, 等. 内埋武器高速风洞弹射投放模型试验关键技术研究[J]. 力学学报, 2018, 50(6): 1346-1355. [109] KEEN K, MORGRET C, LANGHAM T, et al. Trajectory simulations should match flight tests and other lessons learned in 30 years of store-separation analysis[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. [110] ÖZGÜR O, ÇETINER A E, YAGIZ B, et al. Store separation analyses by means of response surface modeling[C]//34th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2016. [111] LIN J Z, WANG X, ZHONG J, et al. Investigation and application of high Mach number multi-body separation test technique[J]. Journal of Propulsion Technology, 2020, 41(4): 925-933 (in Chinese). 林敬周, 王雄, 钟俊, 等. 高马赫数多体分离试验技术研究与应用[J]. 推进技术, 2020, 41(4): 925-933. [112] FLORA T J, REEDER M F, LOFTHOUSE A, et al. Dynamic store release of ice models from a cavity into Mach 2.9 flow[J]. Journal of Aircraft, 2014, 51(6): 1927-1941. [113] CENKO A, PHILLIPS K, M HOLMES I. Captive Trajectory System sting effects on store loads[C]//32nd Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1994. [114] JIN X, YUAN B, ZHANG L Z, et al. A technique of separation trajectory test for stores with folding wing[J]. Journal of Experiments in Fluid Mechanics, 2014(1): 80-84 (in Chinese). 金鑫, 袁兵, 张利珍, 等. 一种折叠弹翼存储物的分离轨迹试验技术[J]. 实验流体力学, 2014(1): 80-84. [115] GUAN D H, CAI W M. Spoiler's effect on the yawing attitude angle of the missile in the bay[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(4): 942-947 (in Chinese). 管德会, 蔡为民. 扰流板对内埋导弹偏航姿态角的影响[J]. 航空学报, 2014, 35(4): 942-947. [116] DONG J G, XIE F, ZHANG C K, et al. Gravity effects of light model method in wind tunnel model drop-test[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 523434 (in Chinese). 董金刚, 谢峰, 张晨凯, 等. 风洞模型投放试验轻模型法重力效应影响[J]. 航空学报, 2020, 41(6): 523434. [117] LORAN WINGFIELD I. Staging evaluation of a two-stage-to-orbit vehicle at Mach 8[C]//10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2001. [118] WOODS W C, HOLLAND S D, DIFULVIO M. Hyper-X stage separation wind-tunnel test program[J]. Journal of Spacecraft and Rockets, 2001, 38(6): 811-819. [119] ARUNAJATESAN S, CHARTRAND C, BIRKBECK R. Analysis of unsteady bay shear layer effects on store separation characteristics[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. [120] COLEY C, LOFTHOUSE A. Correlation of weapon bay resonance and store unsteady force and moment loading[C]//50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2012. [121] BAMBER M L. Two methods of obtaining aircraft store trajectories from wind tunnel investigation: AD233198[R]. Washington, D.C. : David Talyor Model Basin, 1960. [122] RAINEY R W. A wind-tunnel investigation of bomb release at a Mach number of 1.62: NACA RM-L53L29[R]. Washington, D.C. : NACA, 1954. [123] JIANG Z H, SONG W, LU W, et al. Critical problems and applied fields of drop-model testing technique in high speed wind tunnel[J]. Acta Aerodynamica Sinica, 2016, 34(6): 744-749, 802 (in Chinese). 蒋增辉, 宋威, 鲁伟, 等. 高速风洞投放模型试验技术的关键问题及应用领域[J]. 空气动力学学报, 2016, 34(6): 744-749, 802. [124] MURRAY N, JANSEN B, GUI L C, et al. Measurements of store separation dynamics[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. [125] CARTER H S, LEE J B. Investigation of the ejection release of several dynamically scaled bluff internal stores at Mach numbers of 0.8, 1.39, and 1.98: NACA RM-L56H28[R]. Washington, D.C. : NACA, 1956. [126] SANDAHL C A, FAGET M A. Similitude relations for free-model wind tunnel studies of store-dropping problems: NACA TN-3907 93R14088[R]. Washington, D.C. : NACA, 1957. [127] HILSON W F. Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from a 0.086-scale model of a current fighter airplane: NASA TM X-128[R]. Washington, D.C. : NASA, 1959. [128] STEPHENS T, ADAMS R. Wind-tunnel simulation of store jettison with the aid of magnetic artificial gravity: NASA-CR-1955[R]. Washington, D.C. : NASA, 1955. [129] COVERT E E. Wind-tunnel simulation of store jettison with the aid of an artificial gravity generated by magnetic fields[J]. Journal of Aircraft, 1967, 4(1): 48-51. [130] BLACK R L. High-speed store separation-Correlation between wind-tunnel and flight-test data[J]. Journal of Aircraft, 1969, 6(1): 42-45. [131] REED J F, CURRY W H. A comparison between transonic wind-tunnel and full-scale store separation characteristics[J]. Journal of Aircraft, 1969, 6(3): 281-283. [132] MARSHALL J C. Analytic evaluation of the limitations of the various scaling laws for free-drop store separation testing[C]//The Fourth JTCG Aircraft/Stores Compatibility Symposium, 1977. [133] HOLDEN M, SMOLINSKI G, MUNDY E, et al. Experimental studies for hypersonic vehicle design and code validation of unsteady flow characteristics associated with "free flight" shroud and stage seperation, and mode switching[C]//46th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2008. [134] MA X, LIU W, CHEN L, et al. Simulative technology for auxiliary fuel tank separation in a wind tunnel[J]. Chinese Journal of Aeronautics, 2016, 29(3): 608-616. [135] CHIN D Y, GRANLUND K O, MAATZ I, et al. Stochastic store trajectory of ice models with forced ejection from a cavity into supersonic flow[C]//2018 Fluid Dynamics Conference. Reston: AIAA, 2018. [136] MERRICK J D, REEDER M F. Sphere release from a rectangular cavity at Mach 2.22 freestream conditions[J]. Journal of Aircraft, 2016, 53(3): 822-829. [137] C STALMACH J Jr, ROMERO S. Dynamic tests of a submissile dispensing system in a supersonic windtunnel[C]//11th Aerodynamic Testing Conference. Reston: AIAA, 1980. [138] JIANG Z H, SONG W, CHEN N, et al. Hypersonic wind tunnel drop-model test on cover ejection from cargo projectile at large angle of attack[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(5): 42-48 (in Chinese). 蒋增辉, 宋威, 陈农, 等. 高超声速风洞子母弹大迎角抛壳投放试验[J]. 实验流体力学, 2016, 30(5): 42-48. [139] SONG W, LU W, JIANG Z H. Wind tunnel drop model test of nose cap separation of supersonic vehicle[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(6): 45-50, 70 (in Chinese). 宋威, 鲁伟, 蒋增辉. 超声速飞行器头罩分离风洞投放模型试验[J]. 实验流体力学, 2017, 31(6): 45-50, 70. [140] SONG W, ZHANG N, ZHU J, et al. Research status and application of wind tunnel drop test technology: review[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(6): 024417 (in Chinese). 宋威, 张宁, 朱剑, 等. 风洞投放试验技术的研究现状与应用综述[J]. 航空学报, 2021, 42(6): 024417. [141] LARSON H, MCDEVITT J. A technique for launching free-flying models in conventional wind tunnels[C]//2nd Aerodynamic Testing Conference. Reston: AIAA, 1966. [142] LAUMANN E. Free-flight multi-body test techniques[C]//2nd Aerodynamic Testing Conference. Reston: AIAA, 1966. [143] JIANG Z H, XUE F, LU W, et al. Critical problems of unsteady wind tunnel test technique on multi-bodies separation[J]. Acta Aerodynamica Sinica, 2019, 37(5): 715-721 (in Chinese). 蒋增辉, 薛飞, 鲁伟, 等. 非定常多体分离风洞试验技术几个关键问题[J]. 空气动力学学报, 2019, 37(5): 715-721. [144] JIANG Z H, SONG W, LU W. High-speed wind tunnel free-flight test technique[J]. Acta Aerodynamica Sinica, 2017, 35(5): 680-686, 692 (in Chinese). 蒋增辉, 宋威, 鲁伟. 高速风洞模型自由飞试验技术[J]. 空气动力学学报, 2017, 35(5): 680-686, 692. [145] CENKO A, CENKO A, PIRANIAN A, et al. Utilizing flight test telemetry data to improve store trajectory simulations[C]//21 st AIAA Applied Aerodynamics Conference. Reston: AIAA, 2003. [146] DAVIDS S, CENKO A. Grid based approach to store separation[C]//19th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2001. [147] ATKINS D. Flight test results of a GBU-38 separating from the B-1B aircraft[C]//46th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2008. [148] SARIGUL-KLIJN M, SARIGUL-KLIJN N, MORGAN B, et al. Flight testing of a new earth-to-orbit air launch method[J]. Journal of Aircraft, 2006, 43(3): 577-583. [149] SPAHR H R. Theoretical store separation analyses of a prototype store[J]. Journal of Aircraft, 1975, 12(10): 807-811. [150] CENKO A. Experience in the use of computational aerodynamics to predict store release characteristics[J]. Progress in Aerospace Sciences, 2001, 37(5): 477-495. [151] ZENG L F, LI J, WANG T Q, et al. Simulation and optimization of the separation process for UAV[J]. Physics of Gases, 2022, 7(4): 9-13 (in Chinese). 曾丽芳, 黎军, 王天琪, 等. 无人机投放分离特性仿真与优化[J]. 气体物理, 2022, 7(4): 9-13. |
[1] | . Effect of distributed ablation pattern on hypersonic flat plate boundary-layer instability [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[2] | . Rapid Prediction Method for Trailing Edge Scattering Noise Applicable to Both Water and Air [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[3] | . Similarity law study of high-lift device noise based on large-scale wind tunnel test [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[4] | Youde XIONG, Chuangchuang LI, Zhenhui ZHANG, Jie WU. Measurement of freestream disturbance in hypersonic wind tunnel with hot-wire anemometer [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 129042-129042. |
[5] | Xu-Qi ZHANG Yu Liu. Experimental study of aerodynamic noise from polygonal cylinders [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[6] | . Experimental study of bionic flow control of separated shear flow [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[7] | Zhangbo CAI, Zhengyu ZHANG, Hao YU, Shuheng ZHAN. Adaptive fast optical flow solution to velocity field of fluorescent oil film [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 128047-128047. |
[8] | . Preliminary experimental study on hypersonic boundary layer stability of HyTRV lift body [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0. |
[9] | Weiqing LAI, Jiuqing WAN. Distributed relative positioning of aircraft group based on path⁃sum algorithm [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 328735-328735. |
[10] | Guoqiang LI, Kuihui SONG, Chen QIN, Guangyin ZHAO, Linxin WU, Yongdong YANG. Test on active control of airfoil dynamic stall based on trailing edge flap [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 128699-128699. |
[11] | Xueliang LI, Chuangchuang LI, Wei SU, Jie WU. Experiment of influence of distributed roughness elements on hypersonic boundary layer instability [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128627-128627. |
[12] | Haixing LI, Feng ZHOU, Wei YAN, Feng BAI, Keliang ZHAO. Effects of roughness ice on aerodynamic performance of civil aircraft horizontal tail [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128657-128657. |
[13] | Yu LIU, Mengjie QIN, Qiang WANG, Xian YI. Scaling law for salty sea spray icing wind tunnel test [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729297-729297. |
[14] | Fan LIU, Xia HUANG, Shuai MA, Lu ZHANG, Xingda CUI, Xinbiao BAO. Simulation framework for hose-drogue aerial refueling system based on MBD-CFD method [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 628408-628408. |
[15] | Xia HUANG, Fan LIU, Zhitao LIU, Jinhua WU. Correlation between numerical simulation and wind tunnel test results of soft refueling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 628447-628447. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341