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HomeInternational Journal of Engineering Research in...International Journal of Engineering Research in...Drag Reduction Technology of Jet - A Review

Drag Reduction Technology of Jet - A Review

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Abstract:

With the development of world’s economy, energy shortage gradually appears. Resistance has a great influence on energy consumption. In other words, drag reduction means saving energy. Development of the drag reduction technology plays a very important role to improve the energy efficiency. Therefore, drag reduction technology of jet has become a hot research field. Drag reduction technology of jet is applied on the surface, so as to reduce surface friction resistance. Through analyzing the necessity of energy efficiency increase and jet drag reduction theory improvement, research progress of lateral jet flow technology and drag reduction technology of jet in the field of aircraft are reviewed. Besides, a main trend on the drag reduction technology of jet research is presented.

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International Journal of Engineering Research in Africa Vol. 17

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International Journal of Engineering Research in Africa (Volume 17)

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30-42

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https://doi.org/10.4028/www.scientific.net/JERA.17.30

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Online since:

July 2015

Authors:

Yunqing Gu, Tian Xing Fan, Jie Gang Mou*, Deng Hao Wu, Shui Hua Zheng, Lan Fang Jiang

Keywords:

Aircraft, Drag Reduction, Lateral Jet, Shock Wave, Votex

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] Chamorro L P, Arndt R E A, Sotiropoulos F. Drag reduction of large wind turbine blades through riblets: Evaluation of riblet geometry and application strategies. Renewable Energy, 2013, 50, pp.1095-1105.

DOI: 10.1016/j.renene.2012.09.001

[2] Chen H W, Rao F G, Shang X P, Zhang D Y, Hagiwarab I. Biomimetic drag reduction study on herringbone riblets of bird feather. Journal of Bionic Engineering, 2013, 10(3), pp.341-349.

DOI: 10.1016/s1672-6529(13)60229-2

[3] Ke G X, Pan G, Huang Q G, Hu H B, Liu Z Y. Reviews of underwater drag reduction technology. Advances in Mechanics, 2009, 39(5), pp.546-554.

[4] Koeltzsch K, Dinkelacker A, Grundmann R. Flow over convergent and divergent wall riblets. Experiments in Fluids, 2002, 33(2), pp.346-350.

DOI: 10.1007/s00348-002-0446-3

[5] Srivastava B. Lateral jet control of a supersonic missile: computational and experimental comparisons. Journal of Spacecraft and Rockets, 1998, 35(20), pp.140-146.

DOI: 10.2514/2.3321

[6] Yang Y G, Zhang Q H, Liu J. Aerodynamic interaction research of perfect gas lateral jet in hypersonic external flow. Acta Aerodynamica Sinica, 2005, 23(3), pp.299-306.

[7] Wu H L, Chen T K, Luo Y S, Gong W Q. Digital particle imaging velocimetre experimental study of the jet to crossflow in a T junction with a sleeve tube. Journal of Xi'an Jiaotong University, 2002, 36(9), pp.886-889.

[8] Gruber M R, Goss L P. Surface pressure measurements in supersonic transverse injection flowfields. Journal of Propulsion and Power, 1999, 15(5), pp.633-641.

DOI: 10.2514/2.5487

[9] Srivastava B. Asymmetric divert jet performance of a supersonic missile computational and experimental comparisons. Journal of Spacecraft and Rockets, 1999, 36(5), pp.621-632.

DOI: 10.2514/2.3490

[10] Sun D C, Hu C B, Cai T M. Computation of supersonic turbulent flowfield with transverse injection. Applied Mathematics and Mechanics, 2002, 23(1), pp.99-105.

[11] Jiang G S, Shu C W. Efficient implementation of weighted ENO schemes. Journal of Computational Physics, 1996, 126(1), pp.202-228.

DOI: 10.1006/jcph.1996.0130

[12] Guan H, Wu C J. Characteristics of vortex structures for large-eddy simulation of turbulent jets in crossflow. Science in China Ser. G Physics, Mechanics & Astronomy, 2006, 36(6), pp.662-677.

DOI: 10.1007/s11433-007-0005-2

[13] Gao X D, Wu X S, Wang X M. A numerical study on high-speed spinning and lateral jet flow field. Journal of Ballistics, 2005, 17(2), pp.8-12.

[14] Xiao Z Y, Mou Bin, Chen Z B, Liu G. Compressible simulation of active flow control using synthetic jets. Acta Aerodynamica Sinica, 2006, 24(1), pp.46-49.

[15] Cai J S, Liu Q H. Numerical investigation of lateral jets in supersonic cross-flows. Acta Aerodynamica Sinica, 2010, 28(5), pp.553-558.

[16] Zhang W, Lin Y F, Chen P J. The investigation of active control technology in airfoil flow field based on the synthetic jet. Helicopter Technique, 2010, 1, pp.15-20.

[17] Chen J Q, Jiang D W, Zhang Y F. The study on the precision of numerical simulation for lateral jets flow and the experiment validation. Acta Aerodynamica Sinica, 2010, 28(4), pp.421-425.

[18] Chen J Q, Zhang Y F, Jiang D W, Mao M L. Numerical simulation of complex flow with multi lateral jets interactions. Chinese Journal of Theoretical and Applied Mechanics, 2008, 40(6), pp.735-743.

[19] Liu J, Yang Y G. Numerical simulation of lateral jet control induced by impulse rocket motor for a supersonic missile. Acta Aerodynamica Sinica, 2005, 23(1), pp.25-28.

[20] Liu J, Yang Y G. Numerical simulation of lateral jet control of a hypersonic missile. Acta Aerodynamica Sinica, 2004, 22(3), pp.309-312.

[21] Yang Y G, Liu J. Unsteady characteristic research of lateral jet in hypersonic external flow. Acta Aerodynamica Sinica, 2004, 22(3), pp.295-302.

[22] Weston P R, Thames F C. Properties of aspect-ratio-4. 0 rectangular jets in a subsonic cross-flow. Journal of Aircraft, 1979, 16(10), pp.701-707.

DOI: 10.2514/3.58592

[23] Barber M, Schetz J, Roe L. Normal sonic helium injection thorough a wedge shaped orifice into a supersonic flow. Journal of Propulsion and Power, 1997, 13(2), pp.257-263.

DOI: 10.2514/2.5157

[24] Cortelezzi L, Karagozian A R. On the formation of the counter-rotating vortex pair in transverse jets. Journal of Fluid Mechanics, 2001, 446, pp.347-373.

DOI: 10.1017/s0022112001005894

[25] Kelso R M, Lim T T, Perry A E. An experimental study of round jets in cross-flow. Journal of Fluid Mechanics, 1996, 306, pp.111-144.

DOI: 10.1017/s0022112096001255

[26] Yuan L L, Street R L, Ferziger J H. Large-eddy simulations of a round jet in crossflow. Journal of Fluid Mechanics, 1999, 379, pp.71-104.

DOI: 10.1017/s0022112098003346

[27] Rivero A, Ferré J A, Giralt F. Organized motions in a jet in crossflow. Journal of Fluid Mechanics, 2001, 444, pp.117-149.

DOI: 10.1017/s0022112001005407

[28] Lim T T, New T H, Luo S C. On the development of large-scale structures of a jet normal to a cross flow. Physics of Fluids, 2001, 13(3), pp.770-775.

DOI: 10.1063/1.1347960

[29] Graham M J, Weinacht P. Numerical investigation of supersonic jet interaction for axisymmetric bodies. Journal of Spacecraft and Rockets, 2000, 37(5), pp.675-683.

DOI: 10.2514/2.3617

[30] Mahmud Z, Bowersox R D W. Aerodynamics of low-blowing-ratio fuselage injection into a supersonic freestream. Journal of Spacecraft and Rockets, 2005, 42(1), pp.30-37.

DOI: 10.2514/1.4803

[31] Min B Y, Lee J W, Byun Y H. Numerical investigation of the shock interaction effect on the lateral jet controlled missile. Aerospace Science and Technology, 2006, 10(5), pp.385-393.

DOI: 10.1016/j.ast.2005.11.013

[32] Meyer B, Nelson H F, Riggins D. Hypersonic drag and heat-transfer reduction using a forward-facing jet. Journal of Aircraft, 2001, 38(4), pp.680-684.

DOI: 10.2514/2.2819

[33] Geng X R, Gui Y W, Wang A L, He L X. Numerical investigation on drag and heat-transfer reduction using 2-D planar and axisymmetrical forward facing jet. Acta Aerodynamica Sinica, 2006, 24(1), pp.85-89.

[34] Geng X R, Gui Y W, He L X, Wang A L. Investigation on hypersonic heat-transfer reduction using an upstream-directed jet. Proceedings of the 3rd International Symposium on Heat Transfer and Energy Conservation, Guangzhou, 2004, 1, pp.18-21.

[35] Shi Q, Li H. Numerical simulation about the effects of flow control for increasing lift and decreasing drag. Acta Aerodynamica Sinica, 2011, 29(3), pp.280-287.

[36] Endwell O D, Victor E P, Wang Ten-see, Ota D K, Blankson I M, Auslender A H. Dynamics of shock dispersion and interactions in supersonic freestreams with counterflowing jets. AIAA Journal, 2009, 47(6), pp.1313-1326.

DOI: 10.2514/1.30084

[37] Ganiev Y C, Gardeev V P, Krasilinikov A V, Lagutin V I, Otmennikov V N, Panasenko A V. Aerodynamic drag reduction by plasma and hot-gas injection. Journal of Thermophysics and Heat Transfer, 2000, 14(1), pp.10-17.

DOI: 10.2514/2.6504

[38] Shang J S, Haes J, Menart J. Hypersonic flow over a blunt body with plasma injection. Journal of spacecraft and rocket, 2002, 39(3), pp.367-375.

DOI: 10.2514/2.3835

[39] Venukumar B, Jagadeesh G, Reddy K P J. Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow. Physics of Fluids, 2006, 18(11), pp.118104-4.

DOI: 10.1063/1.2401623

[40] Fomin V M, Maslov A A, Malmuth N D, Fomichev V P, Shashkin A P, Korotaeva T A, Shiplyuk A N, Pozdnyakov G A. Influence of a counterflow plasma jet on supersonic blunt-body pressures. AIAA Journal, 2002, 40(6), pp.1170-1177.

DOI: 10.2514/3.15178

[41] Chen L W, Wang G L, Lu X Y. Numerical investigation of a jet from a blunt body opposing a supersonic flow. Journal of Fluid Mechanics, 2011, 684, pp.85-110.

DOI: 10.1017/jfm.2011.276

[42] Zhou C Y, Ji W Y, Zhang X W, Deng L J. Numerical investigation on counter-flow jet drag reduction of a bluff body in supersonic flow. Chinese Journal of Applied Mechanics, 2012, 29(2), pp.159-163.

[43] He K F, Dong W Z, Chen J Q, Deng X G. Numerical studies of flowfields around the supersonic blunt body with the jet of the mixture of air and kalium. Acta Aerodynamica Sinica, 2006, 24(1), pp.90-94.

[44] Wang X, Pei X, Chen Z M, Xu M. Supersonic with counter-flowing jets on drag and heat-transfer reduction. Journal of Propulsion Technology, 2010, 31(3), pp.261-264.

[45] He K, Chen J Q, Dong W Z. Penetration mode and drag reduction research in hypersonic flows using a counter-flow jet. Chinese Journal of Theoretical and Applied Mechanics, 2006, 38(4), pp.438-445.

[46] Yang Y, Liu X Q, Asif S. Transonic drag reduction on supercritical wing section using shock control bumps. Transactions of Nanjing University of Aeronautics & Astronautics, 2012, 29(3), pp.207-214.

[47] Eswar J, Mark P, William B B. Applications of a counterflow drag reduction technique in high-speed systems. Journal of Spacecraft and Rockets, 2002, 39(4), pp.605-614.

DOI: 10.2514/2.3850

[48] Bushnell D M. Shock wave drag reduction. Annual Review Fluid Mechanics, 2004, 36(1), pp.81-96.

DOI: 10.1146/annurev.fluid.36.050802.122110

[49] Jiang Z L, Liu Y F, Han G L, Zhao W. Experimental demonstration of a new concept of darg reduction and thermal protection of hypersonic vehicles. Acta Mechanic Sinica, 2009, 25(3), pp.417-419.

DOI: 10.1007/s10409-009-0252-8

[50] Yonezawa M, Yamashita H, Obayashi S. Investigation of supersonic wing shape using Busemann biplane airfoil. Collection of Technical Papers-45th AIAA Aerospace Sciences Meeting, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2007, 12, pp.8482-8492.

DOI: 10.2514/6.2007-686

[51] Kusunose K. A fundamental study for the development of boomless supersonic transport aircraft. Collection of Technical Papers-44th AIAA Aerospace Sciences Meeting, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2006, 11, pp.7785-7807.

DOI: 10.2514/6.2006-654

[52] Maruyama D, Matsuzawa T. Consideration at off-design conditions of supersonic flows around biplane airfoils. Collection of Technical Papers-45th AIAA Aerospace Sciences Meeting, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2007, 12, pp.8493-8513.

DOI: 10.2514/6.2007-687

[53] Hua R H, Ye Z Y. Drag reduction method for supersonic missile based on Busemann biplane concept. Chinese Journal of Applied Mechanics, 2012, 29(5), pp.535-540.

[54] Fu Q. The slender body theory and its application on decreasing the drag in transonic flow. Engineering Mechanics, 1999, 16(3), pp.64-69.

[55] Tian T, Yan C. Numerical simulation on opposing jet in hypersonic flow. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(1), pp.9-12.

[56] Wang J F, Wu Y Z. Numerical simulation for hypersonic flow on unstructured grid and analysis of drag induction effects on channel-configuration. Journal of Nanjing University of Aeronautics & Astronautics, 2004, 36(6), pp.671-676.

[57] Miles R B, Macheret S O, Shneider M N, Steeves C, Murray R C, Smith T, Zaidi S H. Plasma-enhanced hypersonic performance enabled by MHD power extraction. 43rd AIAA Aerospace Sciences Meeting and Exhibit-Meeting Papers, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2005, pp.13175-13190.

DOI: 10.2514/6.2005-561

[58] Menart J, Shang J, Atzbach C, Magoteaux S, Slagel M, Bilheimer B. Total drag and lift measurements in a Mach 5 flow affected by a plasma discharge and a magnetic field. 43rd AIAA Aerospace Sciences Meeting and Exhibit-Meeting Papers, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2005, pp.15903-15918.

DOI: 10.2514/6.2005-947

[59] Geng Y F, Yan C. Numerical investigation of self-aligning spiked bodies at hypersonic speeds. Chinese Journal of Theoretical and Applied Mechanics, 2011, 43(3), pp.441-446.

[60] Riggings D, Johnson E, Nelson H F. Blunt body wave drag reduction using focused energy deposition. AIAA Journal, 1999, 37(4), pp.460-467.

DOI: 10.2514/3.14192

[61] Georgievsky P Y, Levin V A. Effective flow-over-body control by energy input upstream. 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 2003, pp.2003-38.

DOI: 10.2514/6.2003-38

[62] Satheeshl K, Jagadeesh G. Experimental investigations on the effect of energy deposition in hypersonic blunt body flow field. Shock waves, 2008, 18(1), pp.53-70.

DOI: 10.1007/s00193-008-0140-3

[63] Mehta R C. Numerical heat transfer study over spiked blunt bodies at Mach 6. 80. Journal of Spacecraft and Rockets, 2000, 37(5), pp.700-703.

DOI: 10.2514/2.3622

[64] Yan C, Gao R, Li J. A new method for estimating the first normal grid spacing in heat flux computations. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, US: American Institute of Aeronautics and Astronautics Inc., 2009, pp.2009-832.

DOI: 10.2514/6.2009-832

[65] Kobayashi H, Maru Y, Fukiba K. Experiment study on aerodynamic characteristics of telescopic aerospikes with multiple disks. Journal of spacecraft and Rockets, 2007, 44(1), pp.33-41.

DOI: 10.2514/1.25250

[66] Geng Y F, Yan C. Numerical investigation on drag and heat-transfer reduction using combined spike and forward facing jet method. Acta Aerodynamica Sinica, 2010, 28(4), pp.436-440.

[67] Srulijes J, Gnemmi P, Seiler F, Runne K. Shock tunnel high speed photography and CFD calculations on spike-tipped bodies. 25th International Congress on High-Speed Photography and Photonics, Beaune, France: SPIE, 2002, 4948, pp.658-670.

DOI: 10.1117/12.516788

[68] Gnemmi P, Srulijes J, Roussel K, Runne K. Flowfield around spike-tipped bodies for high attack angles at Mach 4. 5. Journal of spacecraft and Rockets, 2003, 40(5), pp.622-631.

DOI: 10.2514/2.6910

[69] Schülein E. Wave drag reduction approach for blunt bodies at high angles of attack: proof-of-concept experiments. 4th AIAA Flow Control Conference, Seattle, WA, US: American Institute of Aeronautics and Astronautics Inc., 2008, pp.2008-4000.

DOI: 10.2514/6.2008-4000

[70] Bletzinger P, Ganguly B N, Wie D V, Garscadden A. Plasmas in high speed aerodynamics. Journal of Physics D: Applied Physics, 2005, 38(4), pp.33-57.

DOI: 10.1088/0022-3727/38/4/r01

[71] Sun Z X. Progress in plasma assisted drag reduction technology. Advances in Mechanics, 2003, 33(1), pp.87-94.

[72] Hartley C S, Portwood T W, Filippelli M V, Myrabo L N, Nagamatsu H T, Shneider M N, Razier Y P. Experimental and computational investigation of drag reduction by electric-arc airspikes at Mach 10. Proceeding of 3rd International Symposium on Beamed Energy Propulsion, New York, 2005, pp.499-513.

DOI: 10.2514/6.2004-35

[73] Misiewicz C, Myrabo L N, Shneider M N. Combined experimental and numerical investigation of electric-arc airspikes for blunt body at Mach 3. Proceeding of 3rd International Symposium on Beamed Energy Propulsion, New York, 2005, pp.528-541.

DOI: 10.1063/1.1925172

[74] Luo J L, Xu M, Dai W Y, Liu Z. Numerical simulation investigation on plasma injection for drag reduction of hypersonic vehicle. Journal of Astronautics, 2009, 30(1), pp.119-122.

[75] Mao M L, Dong W Z, Deng X G, Chen J Q. Numerical simulation study of the interaction between a high-powered laser and the hypersonic flowfield about a spherecone. Acta Aerodynamica Sinica, 2001, 19(2), pp.172-176.

[76] Li Q, Jin X, Cao Z R, Huang H. Effects on aerodynamic drag of incident laser energy in technology of laser plasma point source drag reduction. Journal of Propulsion Technology, 2010, 31(3), pp.377-380.

[77] Ganiev Y C, Gordeev V P, Krasilnikov A V, Lagutin V I, Otmennikov V N, Panasenko A V. Theoretical and experimental study of the possibility of reducing aerodynamic drag by employing plasma injection. 37th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, US: American Institute of Aeronautics and Astronautics Inc., 1999, pp.1999-0603.

DOI: 10.2514/6.1999-603