1. 中国民用航空飞行学院 空中交通管理学院, 广汉,618307
2. 四川航空股份有限公司 运行风险控制中心,成都,610202
潘卫军(1968-), 男, 湖北黄冈人, 教授, 院长, 研究方向:空中交通管理、飞机空气动力学、计算机仿真等.E-mail:deepblue9001@163.com
纸质出版:2019
移动端阅览
潘卫军, 栾天, 康贤彪, 张庆宇, 任杰, 张强. 飞机尾流观测研究进展[J]. 空气动力学学报, 2019, 37(4): 511-521.
PAN Weijun, LUAN Tian, KANG Xianbiao, et al. Progress in observational studies of aircraft wake vortex in ground proximity[J]. 2019, 37(4): 511-521.
潘卫军, 栾天, 康贤彪, 张庆宇, 任杰, 张强. 飞机尾流观测研究进展[J]. 空气动力学学报, 2019, 37(4): 511-521. DOI: 10.7638/kqdlxxb-2018.0136.
PAN Weijun, LUAN Tian, KANG Xianbiao, et al. Progress in observational studies of aircraft wake vortex in ground proximity[J]. 2019, 37(4): 511-521. DOI: 10.7638/kqdlxxb-2018.0136.
飞机尾流观测试验是研究飞机尾流演化耗散行为的基础。受到不同大气环境的影响,针对巡航、进近等阶段的飞机尾流观测具备一定的挑战性。本文综述了以风洞和拖曳水池为主的飞机尾流实验室观测,以及以激光雷达及微波雷达为主的飞机尾流现场观测的研究成果和研究进展。尾流的风洞观测试验能较好地实现对近区内飞机尾流卷起、发展、脱落,特别是对近区内尾流合并过程(包括飞机翼尖涡、襟翼涡、水平尾翼涡、发动机喷流间的合并)的观测;尾流的拖曳水池观测试验能较好地实现对飞机尾流在扩展近区、及中区内演化过程的观测。尾流的现场观测试验能有效地获取飞机尾流在真实大气背景场中的演化耗散过程,从而为研究不同大气背景条件对飞机尾流的影响,并进而建立飞机尾流动态间隔标准提供重要参考。
Observational experiment of aircraft wake vortex is the basis of studying the evolution behavior of aircraft wake vortex. Disturbed by the effects of atmospheric environment
the exact observation of aircraft wake vortex in cruising and approaching is challenging. In this paper
the laboratory wake observation method including the wind tunnel and towing tank experiment
and the in-site observation method using laser radar and microwave radar equipment has been discussed. The wind tunnel experiment is able to capture the roll-up
development
fall out of the aircraft wake vortex as well as vortices merging (including merging among the wing tip vortex
flap vortex
horizontal tailplane vortex
jet-flow
etc.)
while the towing tank experiment can well capture the evolution behavior of aircraft wake vortex in the extended near field and mid field. In addition
the in-situ observational experiment can well capture the process of evolutionary dissipation of aircraft wake vortices in the atmospheric environment
so it can be served as an important reference for studying the effect of different atmospheric environment on the evolution process of aircraft wake vortices
and further for establishing the dynamic separation standard of aircraft wake vortex.
ZHOU B. Study on the microstructure and scattering characteristics of aircraft wake vortices[D]. Changsha: National University of Defense Technology, 2009. (in Chinese)
ZHOU B, WANG X S, WANG T, et al. Influence of cross wind speeds on aircraft wake vortex movement[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(5):773-779. (in Chinese)
HALLOCK J N, HOLZÄPFEL F. A review of recent wake vortex research for increasing airport capacity[J]. Progress in Aerospace Sciences, 2018, 98:27-36.
GERZ T, HOLZÄPFEL F, DARRACQ D. Commercial aircraft wake vortices[J]. Progress in Aerospace Sciences, 2002, 38(3):181-208.
ZHU D W. Analysis of velocity model of aircraft wake vortex[J]. Journal of Civil Aviation Flight University of China, 2005, 16(6):17-20. (in Chinese)
Summary Report: XB-70 Accident Investigation[R]. USAF, 1966.
PAN W J. Foundation of air traffic management[M]. Chengdu:Southwest Jiaotong University Press, 2013. (in Chinese)
HALLOCK J, SOARES M. Is the B757 Really a "Heavy" Aircraft?[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. 2007: 288.
LIN M D, CUI G X, ZHANG Z S, et al. Large eddy simulation on the evolution and the fast-time prediction of aircraft wake vortices[J]. Chinese Journal of Theoretical and Applied Mechanics, 2017, 49(06):1185-1200. (in Chinese)
AN C J, LIU C W. The influence of aircraft wake vortex on air safety[J]. Flight Dynamics, 2000, 18(4):69-72. (in Chinese)
LI C S, LENG Z C. Wake, the aircraft's killer[J]. China Civil Aviation, 2001, 12:44-44. (in Chinese)
HE D F. Safety effect and precautions for flowing aircraft by leading aircraft wake vortices[J]. Journal of Civil Aviation Flight University of China, 2005, 16(1):12-19. (in Chinese)
SUN H, HU M H, ZHANG Y, et al. Research of miles in trail strategy in sector boundary based on genetic algorithm[J]. Journal of Transportation Systems Engineering and Information Technology, 2010, 10(6):174-179. (in Chinese)
ZHAO M, WANG X L. Sector flow management decision-making based on MIT[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(S1):136-140.
WU X P, YANG H Y, HAN S C. Analysis of properties and delay propagation of air traffic based on complex network[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(S1):113-119. (in Chinese)
MA Y Y, HU M H, YIN J N, et al. Collaborative sequencing and scheduling method for arrival and departure traffic flow in multi-airport terminal area[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(02):225-237. (in Chinese)
MARSHALL R E, ASHOK M, VICKI L H W, et al. Three-centimeter doppler radar observations of wingtip-generated wake vortices in clear air[R]. NASA/CR-97-206260, 1997.
DARRACQ D, CORJON A, FRÉ, et al. Simulation of wake vortex detection with airborne Doppler lidar[J]. Journal of Aircraft, 2000, 37(6):984-993.
HOLZÄPFEL F, GERZ T, KÖPP F, et al. Strategies for circulation evaluation of aircraft wake vortices measured by lidar[J]. Journal of Atmospheric and Oceanic Technology, 2003, 20(8):1183-1195.
BARBARESCO F, JUGE P, BRUCHEC P, et al. Eddy dissipation rate (EDR)retrieval with ultra-fast high range resolution electronic-scanning X-band airport radar: Results of European FP7 UFO Toulouse airport trials[C]//Radar Conference (EuRAD), 2015 European. IEEE, 2015: 145-148.
HOLT J C, GARRY K P. Dynamic wind tunnel simulation of aircraft wake vortex trajectory in ground proximity[C]//54th AIAA Aerospace Sciences Meeting. 2016: 1069.
GABOR O, KOREANSCHI A, BOTEZ R M, et al. Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance[J]. Aerospace Science and Technology, 2016, 53:136-153.
MARTÍEZ-ARANDA S, GARCÍA-GONZÁLEZ A L, PARRAS L, et al. Comparison of the aerodynamic characteristics of the NACA0012 airfoil at low-to-moderate reynolds numbers for any aspect ratio[J]. International Journalof Aerospace Sciences, 2016, 4(1):1-8.
MCILWAIN S, CARTER D L, GIVOGUE G, et al. C-17 Globemaster Ⅲ vortex control finlets simulation and wind tunnel testing[C]//35th AIAA Applied Aerodynamics Conference. 2017: 4227.
LAUER N, YEO D W, SNYDER D A, et al. Tip-vortex localization for cross-stream position control of a multi-hole probe relative to a stationary wing in a free-jet wind tunnel[C]//AIAA Guidance, Navigation, and Control Conference. 2017: 1484.
XU X B, SHU H F, XU Y, et al. Experimental investigation on lifting body aerodynamic force with simulated aft-body jet[J]. Acta Aerodynamica Sinica, 2016, 34(1):86-90. (in Chinese)
CROW S C. Stability theory for a pair of trailing vortices[J]. AIAA Journal, 1969, 8(12):2172-2179.
YANG K, HUANG H, XU S J. Experimental study of effects of multi-winglets and tip blowing upon wingtip vortex[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(6):27-38. (in Chinese)
SUN H C, DAICHIN. The influence of the tip sails shape on the wing aerodynamics in ground effect[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(6):10-17. (in Chinese)
HUANG S Q, SHEN G X, KONRATH R, et al. Experimental study of SPIV on controlling wake vortex[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(1):18-22. (in Chinese)
HU Y H, WU Y H. Research on aircraft evolution and the Lidar measurement technology[J]. Infrared and Laser Engineerin, 2011, 40(6):1063-1069. (in Chinese)
STEPHAN A, HOLZÄPFEL F, ZHOLTOVSKI S. The effect of gusts on aircraft wake vortices[J]. Aircraft Engineering and Aerospace Technology, 2017, 89(5):692-702.
PENKIN M S, BOREISHO A S, KONYAEV M A, et al. Detection of the aircraft vortex wake with the aid of a coherent doppler lidar[J]. Journal of Engineering Physics and Thermophysics, 2017, 90:951-957.
PAUGAM R, PAOLI R, CARIOLLE D. Influence of vortex dynamics and atmospheric turbulence on the early evolution of a contrail[J]. Atmospheric Chemistry and Physics, 2010, 10(8):3933-3952.
BIAN Q, NENER B, WANG X. Control parameter tuning for aircraft crosswind landing via multi-solution particle swarm optimization[J]. Engineering Optimization, 2018, 50(11):1914-1925.
KÖRNER S, AHMAD N N, HOLZÄPFEL F, et al. Multimodel ensemble methods for prediction of wake-vortex transport and decay[J]. Journal of Aircraft, 2017, 54(5):1849-1859.
WANG C H J, ZHAO D, SCHLVTER J, et al. LES study on the shape effect of ground obstacles on wake vortex dissipation[J]. Aerospace Science and Technology, 2017, 63:245-258.
AHMAD N N, PROCTOR F. Review of idealized aircraft wake vortex models[C]//52nd Aerospace Sciences Meeting. 2014: 0927.
ELIASON B G, GARTSHORE I S, PARKINSON G V. Wind tunnel investigation of Crow instability[J]. Journal of Aircraft, 1975, 12(12):985-988.
PARKS P C. A new look at the dynamics of vortices with finite cores[C]//OLSEN J H, GOLDBURG A, ROGERS M. Aircraft Wake Turbulence and Its Detection. Springer US, 1971: 355-388.
BABIE B M, NELSON R C. Wavelength and amplitude measurement of an unstable wake vortex bending mode via helium-bubble visualization[C]//Proceedings of the 13th International. Symposium on Flow Visualization. 2008.
BREITSAMTER C. Wake vortex characteristics of transport aircraft[J]. Progress in Aerospace Sciences, 2011, 47(2):89-134.
ALTAF A, THONG T B, OMAR A A, et al. Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing[C]//IOP Conference Series: Materials Science and Engineering. IOP Publishing, 2017, 184(1): 012002.
BRANDON J M, JORDAN F L, STUEVER R A. Application of wind tunnel free-flight technique for wake vortex encounters[R]. NASA Technical Paper, 1997.
LIU Z Y, TAO Y, SHI Z W, et al. Investigation on formation flight in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4):20-25. (in Chinese)
JOHN O H. Results of trailing vortex studies in a towing tank[M]. Aircraft Wake Turbulence and Its Detection. Springer US, 1971: 455-472.
SCARANO F, WIJK C V, VELDHUIS L. Traversing field of view and AR-PIV for mid-field wake vortex investigation in a towing tank[J]. Experiments in Fluids, 2002, 33(6):950-961.
BAO F, YANG J W, LIU J S, et al. Experimental study on self-dissipation wake wing based on interactive instability[J]. Chinese Journal of Theoretical and Applied Mechanics, 2015, 47(3):398-405. (in Chinese)
BAO F, LIU J S, ZHU R, et al. Experimental study on Rayleigh-Ludwieg instability of aircraft wake vortex[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(7):2166-2176. (in Chinese)
ZHU R, LIU J S, LIU Z R, et al, Experiment on a new concept wing layout with alleviated wake vortex[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(4):120250. (in Chinese)
VELDHUIS L L M, DE KAT R, ELSINGA G E. Towing tank experiments of cold jet-vortex interaction on a generic wing-flap model[J]. FAR-WAKE Technical report TR, 2006, 2:1-5.
GEGORIO F D, RAGNI A, ALBANO F, et al. Aircraft wake vortex detection in large towing tank[C]//Triennial International Symposium on Fluid Control, Measurement and Visualization, Flucome. 2003.
HUANG S Q, SHEN G S, KONRATH R, et al. Experimental investigation of influence of jets on aircraft wake votices[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(5):899-908.
HALLOCK J, BURNHAM D, HALLOCK J, et al. Decay characteristics of wake vortices from jet transport aircraft[J]. Journal of Aircraft, 2013, 50(1):82-87.
HARRIS M, VAUGHAN J M, HUENECKE K, et al. Aircraft wake vortices:a comparison of wind-tunnel data with field trial measurements by laser radar[J]. Aerospace Science Technology, 2000, 4(5):363-370.
VAUGHAN J M, HARRIS M. Lidar measurement of B747 wakes:observation of a vortex within a vortex[J]. Aerospace Science Technology, 2001, 5(6):409-411.
KÖPP F, RAHM S, SMALIKHO I. Characterization of aircraft wake vortices by 2-μm pulsed doppler lidar[J]. Journal of Atmospheric Oceanic Technology, 2004, 21(2):194-206.
MACKEY S, BURNHAM D. Use of a commercial wind SODAR for measuring wake vortices[C]//27th AIAA Aeroacoustics Conference, 2006: 2537-2547.
BARBARESCO F, JEANTET A, MEIER U. Wake vortex detection monitoring by X-band doppler radar: Paris Orly radar campaign results[C]//Iet International Conference on Radar Systems. IET, 2007: 1-5.
BARBARESCO F, MEIER U. Radar monitoring of a wake vortex:Electromagnetic reflection of wake turbulence in clear air[J]. Comptes Rendus Physique, 2010, 11(1):54-67.
BARBARESCO F, JUGE P, KLEIN M, et al. Optimising runway throughput through wake vortex detection, prediction and decision support tools[C]//Tyrrhenian International Workshop on Digital Communications-Enhanced Surveillance of Aircraft and Vehicles. IEEE, 2011: 27-32.
WU Y H, HU Y H, DAI D C, et al. Research on the technique of aircraft wake vortex detection based on 1.5 μm doppler lidar[J]. Acta Photonica Sinica, 2011, 40(6):811-817. (in Chinese)
XU S L, HU Y H. ZHAO X N, et al. Extrication of wake vortex parameters based on lidar echo[J]. Acta Photonica Sinica, 2013, 42(1):54-58. (in Chinese)
XU S L, HU Y H, GUO L R, et al. Design and performance analysis of aircraft wake vortex coherent laser detection system[J]. Laser Optoelectronics Progress, 2014, 51(8):100-105. (in Chinese)
LI C, LIU J W, ZHOU D F, et al. Correction method of tilt wind field of mobile wind lidar[J]. Laser Technology, 2017, 41(3):385-390. (in Chinese)
WANG X T, LIU B Y, WU S H, et al. 1.55 μm all-fiber laser heterodyne detection and data analysis with high measurement accuracy of velocity[J]. LaserOptoelectronics Progress, 2011, 48(6):8-12. (in Chinese)
ZHANG H W, WANG Q C, WU S H, et al. Low-level win shear observation at Beijing capital international airport based on coherent doppler lidar[J]. Journal of Atmospheric and Environmental Optics, 2018, 13(1):34-41. (in Chinese)
LI J, WANG T, LI W C, et al. Experimental study of X-bang radar scattering characteristics of aircraft wake vortices[J]. Radar Science and Technology, 2009, 7(6):406-410. (in Chinese)
LI J, WANG X S, WANG T, et al. Radar detection performance of aircraft wake vortices in wet air[J]. Radar Science and Technology, 2009, 7(5):333-338. (in Chinese)
LI J, WANG X S, WANG T, et al. Detection performance of aircraft wake vortices with pulse doppler radar[J]., 2010, 05(3):305-310. (in Chinese)
QU L H, WANG X S. Measurement methods of wake vortice scattering characteristics[J]. Chinese Journal of Radio Science, 2012, 2:54-61. (in Chinese)
NIU F L, WANG W, WANG T, et al. Study on radar characteristics for aircraft wake under the rainfall[J]. Journal of Air Force Radar Academy, 2013, 2:95-99. (in Chinese)
GUO C, WANG T, LI J B, et al. Circulation estimation of wake vottex in cloudy and misr conditions[J]. Modern Radar, 2015, 37(6):10-15. (in Chinese)
LI J B, GAO H, WANG T, et al. A survey of the scattering characteristics and detection of aircraft wake vortices[J]. Journal of Radars, 2017, 6(6):653-672. (in Chinese)
WANG T, QU L H, GUO C, et al. The millimeter band Doppler characteristics of wake vortices in cloudy and foggy[J]. Journal of Infrared and Millimeter Waves, 2014, 33(4):412-419. (in Chinese)
LI J B, WANG X S, WANG T, et al. Simulation based velocity circulation of aircraft wake vortex under the rainfall condition with upward looking radar[P]. CN106596039A, 2017. (in Chinese)
HU X X. Update on aircraft wake vortex spacing standards research[J]. China Civil Aviation, 2015, 1:78-80. (in Chinese)
0
浏览量
0
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024621