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民机空气动力设计先进技术

朱自强

朱自强. 民机空气动力设计先进技术[J]. 物理, 2016, 45(10): 651-659. DOI: 10.7693/wl20161005
引用本文: 朱自强. 民机空气动力设计先进技术[J]. 物理, 2016, 45(10): 651-659. DOI: 10.7693/wl20161005
ZHU Zi-Qiang. Advanced aerodynamic design for commercial aircraft[J]. PHYSICS, 2016, 45(10): 651-659. DOI: 10.7693/wl20161005
Citation: ZHU Zi-Qiang. Advanced aerodynamic design for commercial aircraft[J]. PHYSICS, 2016, 45(10): 651-659. DOI: 10.7693/wl20161005

民机空气动力设计先进技术

Advanced aerodynamic design for commercial aircraft

  • 摘要: 文章简要地介绍了两种民机空气动力先进设计技术的概念及其研究进展。一为层流流动主动控制技术。其核心措施是减弱流动的不稳定性,推迟转捩的发生,从而增大层流流动区域。目前混合层流流动控制方法发展比较充分,有望应用于未来民机的设计中。另一为新型非常规布局,包括翼身融合体、支撑机翼、吞吸机身边界层等新型气动布局,这些均有望大大提高未来民机的性能。
    Abstract: The concepts and the research on two kinds of advanced aerodynamic technology are briefly reviewed. One is laminar flow active control, which focuses on increasing the laminar flow region through decreasing flow instability and delaying the transition. A hybrid laminar flow control method has now been developed and probably will be used in future design. The other is a new type of aerodynamic shape, which can greatly increase the performance of commercial transport aircraft. Three new types of configuration——the blended wing body, strut-braced wing,and body boundary layer ingestion will be briefly described.
  • [1] 朱自强,吴宗成,陈迎春等. 民机空气动力学设计先进技术. 上海:上海交通大学出版社,2013
    [2] 李广义,张晋平. 国际航空,2011,2:47
    [3] 温坤. 国际航空,2011,6:67
    [4] 朱自强,鞠胜军,吴宗成. 航空学报,2016,37(7):2065
    [5] Schrauf G. The Aeronautical J.,2005,109(1102):639
    [6] Thibert J J,Reneaux J,Schmitt R V. ONERA activities on drag reduction.ICAS-90-3.6.1,1990
    [7] Liebeck R H. Journal of Aircraft,2004,41(1):10
    [8] Holmes B J,Clifford J,Martin G L et al. Manufacturing tolerances for natural laminar flow airframe surface. SAE paper 850863,1985
    [9] Saric W S,Reed H L,White E B. Annu. Rev. Fluid Mech.,2003,35:413
    [10] Collier F S. An overview of recent subsonic laminar flow control flight experiments. AIAA 93-2987,1993
    [11] Kirchner M E. Laminar flow:challenge and potential. NASACP-2487,part1,1987. 25—44
    [12] Joslin R D. Overview of laminar flow control. NASATP-208705,1998
    [13] Arcara P C,Bartlett D W,Mecullers L A. Analysis for the application of hybrid laminar flow control to a long rang subsonic transport aircraft. SAE Paper 912113,1991
    [14] Wagner R D,Maddalon D V,Fisher D F. Journal of Aircraft,1990,27(3):239
    [15] Maddalon D V. Hybrid laminar flow control flight research.NASATM4331,1991
    [16] Crouch J D. Boundary layer transition prediction for laminar flow control. AIAA 2015-2472,2015
    [17] Bonet J T. Boeing ERA N+2 advanced vehicle concept results.In:50th AIAA aerospace science meeting,Jan.11,2012
    [18] Thomas R H,Burley C L,Olson E D. Hybrid wing body aircraft system noise assessment with propulsion airframe aeroacoustic experiments. AIAA 2010-3913,2010
    [19] 张正国. 国际航空,2010,2:56
    [20] Jameson K K,Marshall D D,Ehrmann R et al. CalPoly’s AMELIA 10 foot span hybrid wing body low noise CESTOL aircraft wind tunnel test and experimental results overview. AIAA-2013-0974,2013
    [21] 朱自强,吴宗成. 航空学报. 2016,37(2):411
    [22] Zeune C H. An overview of the airforce's speed agile concept demonstration program. AIAA 2013-1097,2013
    [23] Gundlach J F,Naghshineh-Pour A H,Gern F et al. Multidisciplinary design optimization and industry review of a 2010 strut-braced wing transonic transport. VPI-MAD99-06-03,1999
    [24] Gern F,Ko A,Grossman B et al. Transport weight reduction through MDO:The strut-braced wing transonic transport. AIAA 2005-4667,2005
    [25] Nam T,Chakraborty I,Gross J et al. Multidisciplinary design optimization of a truss-braced wing concept. AIAA 2014-2423,2014
    [26] Graham W. Trauss-braced wing shows promise. AW&ST,2015-01-12
    [27] Greitzer E M,Bonnefoy P A,Dela R B et al. N+3 Aircraft Concept Designs and Trade Studies,Final Report,Vol1,Vol2,NASA CR-2010-216794,2010
    [28] Mark D. Development of the D8 Transport Configuration. AIAA2011-3970,2011
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出版历程
  • 收稿日期:  2016-09-05
  • 发布日期:  2016-10-11

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