期刊文献+

飞机外挂物投放安全性的参数影响分析 被引量:12

Parameter analysis of safety in store separation
原文传递
导出
摘要 研究了飞机在不同飞行高度、速度和姿态下,不同外挂物质量对投放安全性的影响。采用CFD方法计算外挂物所受气动力,通过六自由度刚体动力学方程计算外挂物的投放轨迹和姿态变化。准定常方法在计算外挂物下落轨迹的每个步长内,认为外挂物和载机都处在定常流场中,载机在投放过程中保持原有运动状态。通过算例给出了典型外挂物在不同速度、高度、姿态下投放的运动轨迹,分析了对安全投放有重要影响的因素,提出了减少外挂物投放风险的建议。 The trajectory of external stores separating from aircraft was computed in different flight conditionswith the quasi-steady method.In every step,the flow fields of external stores and aircraft were regarded as steadyand the aerodynamic forces acting on stores were calculated with the CFD method while keeping in the aircraft flightinitial states.A 6 DOF rigid body model was used to compute the trajectory resulting from the combination of thestores mass properties and aerodynamic loading.Separation of a generic wing-pylon-store configuration was givenand comparisons were demonstrated in flight states of different Mach number,altitude and attitude of aircraft.Thesafe separating effected by elements was concluded,and suggestions about risk-reduction were given.
作者 聂璐 向锦武
出处 《飞行力学》 CSCD 北大核心 2011年第2期25-28,共4页 Flight Dynamics
关键词 外挂物 外挂物分离 准定常 external stores store separation quasi-steady
  • 相关文献

参考文献9

  • 1Arnold R J, Epstein C S. Store separation flight testing [ R]. AGARD-AG-300-Vol ( 5 ), 1986.
  • 2Alex Cenko. Experience in the use of computational aerodynamics to predict store release characteristics [ J]. Progress in Aerospace Science, 2001,37 ( 5 ) :477-495.
  • 3Nathan C Prewitt, Davy M Belk, Wei Shyy. Parallel computing of overset grids for aerodynamic problems with moving objects [ J ]. Progress in Aerospace Science, 2000,36 ( 2 ) : 117-172.
  • 4Roland Glowinski, Tsorng-Whay Pan, Jacques Periaux. Numerical simulation of a multi-store separation phenomenon : a fictitious domain approach [ J]. Computer Methods in Applied Mechanics and Engineering, 2006, 195 (41- 43 ) :5566-5581.
  • 5Debashis Sahoo, Anuradha Annaswamy, Frrukh Alvi. Active store trajectory control in supersonic cavities using microjets and low-order modeling [ J ]. AIAA Journal, 2007,45(3) :516-531.
  • 6彭兢,王衍洋,金长江.飞机外挂物发射/投放运动的数值仿真方法[J].飞行力学,1997,15(3):24-29. 被引量:4
  • 7Sadeh Y, Gaton V A. F-16/SPICE separation analysis- summary of the risk-reduction phase program[J]. Journal of Aircraft ,2003,40( 1 ) :70-75.
  • 8雷娟棉,吴甲生,肖雅彬.母弹近区子弹的弹道特性[J].北京理工大学学报,2006,26(2):95-99. 被引量:2
  • 9Scott M Murman, Michael J Aftosmis, Marsha J Berger. Simulation of store separation from an F/A-18 with a Cartesian method [ J]. Journal of Aircraft,2004,41 (4) :870- 877.

二级参考文献9

  • 1雷娟棉,吴甲生,肖雅彬.布撒器—子弹气动干扰风洞实验研究[J].兵工学报,2005,26(4):535-539. 被引量:10
  • 2樊启发.世界制导兵器手册[M].北京:兵器工业出版社,1996.
  • 3杨启人.子母弹飞行动力学[M].北京:国防工业出版社,1999..
  • 4Stalmach C J,Romero Jr S.Dynamic tests of a submissile dispensing system in a supersonic wind tunnel[R].US:AIAA 80-0452,1980.
  • 5Perkins S,Jr C.Supersonic submunition aerodynamics during dispense[R].US:AIAA 88-0335,1988.
  • 6Lundy T E,Braddock W F.Submissile aerodynamic study during dispense[R].US:AD/A 111778,1989.
  • 7Ross J A.Prediction the effects of aircraft geometry on the carriage and release of external stores[R].US:AIAA 87-0270,1987.
  • 8Culotta A J.A predictive technique for determining store motion after release from a carrier vehicle at supersonic speeds[R].US:AIAA 86-0586,1986.
  • 9Deep R A,Brazzel C Z,Sims J L.Aerodynamics of submissiles during dispense[R].US:AIAA 85-0105,1985.

共引文献4

同被引文献64

引证文献12

二级引证文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部