期刊文献+

新型四分量片式铰链力矩天平研制与应用 被引量:6

Development and Application of a Novel Four Components Plate Type Hinge Moment Balance
下载PDF
导出
摘要 受试验模型和天平结构等条件限制,目前高速风洞片式铰链力矩天平精准度不高,而且难以实现轴向力测量,影响试验数据质量。针对该问题,设计了多柱梁对称元件结构以及新型组合式电桥方案,研制出一种可以有效测量轴向力的四分量片式铰链力矩天平,并成功应用于某飞机模型舵面铰链力矩测力试验。校准数据以及试验结果表明,该天平精准度优于常规片式结构三分量片式天平,能有效提高试验数据质量,有很好的应用价值。 By the limitation of the testing model and balance structure, wind tunnel balance’ s precision and accuracy is lower, and it’ s hard to measure axial force of the control flap in high wind tunnel testing, so the quality of the testing data can be influenced. For solving this question, multi-beam symmetrical structure and a new combined bridge scheme had been designed, finally, a novel four components plate type hinge moment balance had been completed, which can measure axial force efficacious and was used in certain airplane model control flap hinge moment testing successfully. The calibration results and the test data shows that the balance’ s precision and the accuracy is better than normal three components plate type hinge moment balance, use such type of balance can increase the quality of the testing da-ta efficiently which has good application value.
出处 《弹箭与制导学报》 CSCD 北大核心 2015年第2期129-133,共5页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 铰链力矩 风洞试验 风洞天平 hinge moment wind tunnel testing wind tunnel balance
  • 相关文献

参考文献9

二级参考文献19

  • 1张晖,肖京平,杨远志,金华.8m×6m风洞铰链力矩试验技术[J].流体力学实验与测量,2004,18(2):20-24. 被引量:7
  • 2孔德永,吴桂馥.舵面铰链力矩的估算[J].空气动力学学报,2005,23(2):263-266. 被引量:14
  • 3王世红,杨希明.FL-2风洞民机实验技术研究[J].航空科学技术,2005,16(6):30-32. 被引量:4
  • 4[5]MIKHAIL A G.Fin gaps and body slots:effect and modeling for guided projectiles.AIAA-87-0447.
  • 5[6]Improved control surface effectiveness for missile.AIAA-82-0318.
  • 6[7]LIN Wen-fan,MICHAEL D Clark. Factors influencing the accurary of aerodynamic hinge moment prediction.ADA066606.
  • 7[8]Aerodynamics characteristics of controls.AGARD-CP-262.
  • 8[10]BRIGGS M M, READ R E, NIELSEN J E .Wing alone aerodynamics to high angles of attack at subsonic and transonic speeds. ADA 125764,1983.
  • 9[11]STALLINGS R L,LAMB M.Wing alone aerodynamics for high angles of attack at supersonic speeds.NASA TP-1889,1981.
  • 10刘永昌.浅谈应变天平校准方法的比较.气动实验与测量控制,1988,:17-20.

共引文献36

同被引文献41

引证文献6

二级引证文献6

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