基于Busemann双翼的三维高超声速机翼研究

doi:10.7527/S1000-6893.2017.21405

Abstract

Abstract: To study on the performance of the hypersonic wing of Busemann biplane airfoils, a hypersonic wing based on the Busemann biplane airfoil is constructed. The aerodynamic characteristics in the hypersonic flow and the influence of temperature on the natural frequencies of the first six modes are studied. Considering complexity of the hypersonic flow and the variety of the disciplines involved, the Busemann biplane is proved theoretically to be able to improve the lift-to-drag ratio, and then the aerodynamic characteristics of the Busemann biplane in the hypersonic flow and its mechanism of reducing drag, increasing lift, and reducing wing tip vortex are studied by numerical simulation. In addition, the hierarchical theory is used to simplify the complex coupling relationship between the disciplines of hypersonic wings, and the effect of temperature on the mode of the hypersonic Busemann biplane is studied. It is shown that the Busemann biplane can significantly improve the lift-to-drag ratio of wings and weaken the strength of the wing tip vortex:the lift coefficient of the Busemann biplane is increased by 28.95%, the drag coefficient is reduced by 13.58%, and the lift-to-drag ratio is increased obviously by 13.53% of that the diamond monoplane. At the same time, at 1 300℃, the first-order natural frequency of the Busemann biplane increases by 99.8% of that of the diamond wing, showing that Busemann biplane have better ability to resist bending. The first-order natural frequency of the Busemann biplane at 1 300℃ decreases by 34.2% of that at 20℃, indicating that the effect of high temperature on the structural performance of the Busemann biplane cannot be neglected.

Key words: hypersonic, Busemann biplane, three dimensional wing, aerodynamic characteristics, mode

CLC Number:

V211.3

LIU Shuhan, ZHU Zhanxia. Research on three dimensional hypersonic wing based on Busemann biplane[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(6): 121405-121405.

References

[1] SZIROCZAK D, SMITH H. A review of design issues specific to hypersonic flight vehicles[J]. Progress in Aerospace Sciences, 2016, 84:1-28.
[2] BUSEMANN A. Aerodynamic lift at supersonic speeds[C]//The 5th Volta Aerodynamic Conference, 1935.
[3] BUSEMANN A. The relation between minimized drag and noise at supersonic speed[C]//The High-speed Aeronautics Conference, 1955.
[4] PATIDAR V K, YADAV R, JOSHI S. Numerical investigation of the effect of stagger on the aerodynamic characteristics of a Busemann biplane[J]. Aerospace Science & Technology, 2016, 55:252-263.
[5] YAMASHITA H, KURATANI N, YONEZAWA M, et al. Wind tunnel testing on start/unstart characteristics of finite supersonic biplane wing[J]. International Journal of Aerospace Engineering, 2013(6):1-10.
[6] IGRA D, ARAD E. Parametric study of an axisymmetric Busemann biplane configuration[J]. Journal of Aircraft, 2009, 46(6):1930-1937.
[7] MARUYAMA D, KUSUNOSE K, MATSUSHIMA K, et al. Aerodynamic analysis and design of Busemann biplane:Towards efficient supersonic flight[J]. Proceedings of the Institution of Mechanical Engineers Part G:Journal of Aerospace Engineering, 2012, 226(2):217-238.
[8] XU Y Z, XU Z Q, LI S G, et al. A hypersonic lift mechanism with decoupled lift and drag surfaces[J]. Science China:Physics, Mechanics & Astronomy, 2013, 56(5):981-988.
[9] HU R, JAMESON A, WANG Q Q. Adjoint-based aerodynamic optimization of supersonic biplane airfoils[J]. Journal of Aircraft, 2012, 49(3):802-814.
[10] YONEZAWA M, YAMASHITA H, OBAYASHI S, et al. Two-dimensional computational fluid dynamics analysis of hysteresis around supersonic biplane in supersonic flow[J]. Journal of the Japan Society for Aeronautical & Space Sciences, 2009, 57:131-133.
[11] LICHER R M. Optimum two-dimensional multiplanes in supersonic flow[C]//Douglass Aircraft Conference, 1955.
[12] KUSUNOSE K, MATSUSHIMA K, MARUYAMA D. Supersonic biplane-A review[J]. Progress in Aerospace Sciences, 2011, 47:53-87.
[13] 赵承熙,叶正寅,华如豪. 新型目标压力分布下的Licher双翼反设计方法研究[J]. 空气动力学学报, 2015, 33(5):610-616. ZHAO C Y,YE Z Y,HUA R H. Inverse design method for the Licher biplane with a new target pressure distribution[J]. Acta Aerodynamica Sinica, 2015, 33(5):610-616(in Chinese).
[14] ZHAO C X, HUA R H, YE Z Y, et al. Unsteady aerodynamic characteristics of the pitched supersonic biplane[J]. Applied Mechanics & Materials, 2015, 798:523-530.
[15] TIAN Y, AGARWAL R K. Shape optimization of Busemann-type biplane airfoil for drag reduction under non-lifting and lifting conditions using genetic algorithms[M]//Optimization Algorithms-Methods and Applications. 2015.
[16] SUGA Y, YAMAZAKI W. Aerodynamic uncertainty quantification of supersonic biplane airfoil via polynomial chaos approach[C]//AIAA Non-Deterministic Approaches Conference. Reston, VA:AIAA, 2015.
[17] MOELDER S, SZPIRO E J. Busemann inlet for hypersonic speeds[J]. Journal of Spacecraft & Rockets, 2015, 3(8):1303-1304.
[18] MARUYAMA D, MATSUSHIMA K, KUSUNOSE K, et al. Three-dimensional aerodynamic design of low-wave-drag supersonic biplane using inverse problem method[J]. Journal of Aircraft, 2009, 46(6):1906-1918.
[19] YONEZAWA M, OBAYASHI S. Aerodynamic performance of the three-dimensional lifting supersonic biplane[J]. Journal of Aircraft, 2010, 47(3):983-991.
[20] ZHAO C X, CHEN Z H, YE Z Y. Inverse design method for a supersonic ring wing based on the Busemann concept[J]. Applied Mechanics & Materials, 2015, 798:602-608.
[21] 刘枫. 动网格技术研究及其在高超声速流动中的应用[D]. 长沙:国防科学技术大学, 2009. LIU F. Study of moving mesh technology and its application in hypersonic flow[D]. Changsha:University of Defense Technology, 2009(in Chinese).
[22] 刘磊. 高超声速飞行器热气动弹性特性及相似准则研究[D]. 绵阳:中国空气动力研究与发展中心, 2014. LIU L. Study on the characteristics and similarity criteria of aerothermoelasticity for hypersonic vehicle[D]. Mianyang:China Aerodynamics Research and Development Center, 2014(in Chinese).

Research on three dimensional hypersonic wing based on Busemann biplane

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