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Improving the performance of ducted fans for VTOL applications: A review

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Abstract

Ducted fans have been widely used in VTOL aircraft due to the high propulsion efficiency and safety. The efficiency and stability of ducted fans deteriorate in some flight conditions such as hovering in crosswinds or ground effect. It is necessary to optimize the ducted fan’s structures or apply flow control methods for better adaptions to the typical conditions. This paper presents a detailed review on the ducted fan technology for VTOL applications, especially the methods for improving its efficiency and stability. We first simplified the classification categories based on boundary conditions instead of flight conditions, since the new classification method covers more situations and is easier to distinguish flow field characteristics. The flow characteristics, thrust properties and the optimal structures under different boundary conditions were summarized and discussed. Finally, new configurations and flow control methods for increasing the efficiency and stability were introduced. The newly proposed integration design between the ducted fan and the motor was emphasized for increasing the power density of the ducted fans. This review would be helpful to improve our understanding of the relationship between the structures, flow characteristics and thrust properties of ducted fans under different flight conditions, and inspires scientists to design high-efficiency and high-stability propulsion systems with ducted fans.

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References

  1. Luo Y W, Qian Y P, Zeng Z Z, et al. Simulation and analysis of operating characteristics of power battery for flying car utilization. eTransportation, 2021, 8: 100111

    Article  Google Scholar 

  2. Zhang T, Barakos G N. Review on ducted fans for compound rotorcraft. Aeronaut J, 2020, 124: 941–974

    Article  Google Scholar 

  3. Stipa L. Experiments with intubed propellers. NASA Technical Reports Server, 1932

  4. Sacks A H, Burnell J A. Ducted propellers—A critical review of the state of the art. Prog Aerospace Sci, 1962, 3: 85–135

    Article  Google Scholar 

  5. Pereira J L. Hover and wind-tunnel testing of shrouded rotors for improved micro air vehicle design. Dissertation for Dcotoral Degree. College Park: University of Maryland, 2008

    Google Scholar 

  6. Lind R, Nathman J, Gilchrist I. Ducted rotor performance calculations and comparison with experimental data. In: Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, 2006. 1069

  7. Bi N P, Kimmel K R, Haas D J. Performance investigation of ducted aerodynamic propulsors. In: Proceedings of the First International Symposium on Marine Propulsors. Trondheim, 2009

  8. Ko A, Ohanian O, Gelhausen P. Ducted fan UAV modeling and simulation in preliminary design. In: Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit. Hilton Head, 2007. 6375

  9. Han H, Xiang C L, Xu B, et al. Experimental and computational analysis of microscale shrouded coaxial rotor in hover. In: Proceedings of the 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2017. 1092–1100

  10. Mi B G. Numerical investigation on aerodynamic performance of a ducted fan under interferences from the ground, static water and dynamic waves. Aerospace Sci Tech, 2020, 100: 105821

    Article  Google Scholar 

  11. Zhang Y T. Review on research of distributed electric propulsion aircraft power system (in Chinese). Encyclopedia Forum, 2018, 2: 582

    Google Scholar 

  12. Akturk A, Camci C. Experimental and computational assessment of a ducted-fan rotor flow model. J Aircraft, 2012, 49: 885–897

    Article  Google Scholar 

  13. Akturk A, Camci C. Double Ducted Fan (DDF) as a novel ducted fan inlet lip separation control device. In: Proceedings of the International Powered Lift Conference. Philadelphia, 2010. 10

  14. Akturk A, Shavalikul A, Camci C. PIV measurements and computational study of a 5-inch ducted fan for V/STOL UAV applications. In: Proceedings of the 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, 2009. 332

  15. Li L, Huang G P, Chen J, et al. Numerical experiment of tip-jet ducted fans with various nozzles. In: Proceedings of the 53rd AIAA/SAE/ASEE Joint Propulsion Conference. Atlanta, 2017. 5093

  16. Li L, Huang G P, Chen J, et al. Numerical investigation of self-driven fan performance with tip-jet. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2017, 50787: V02AT39A0213

    Google Scholar 

  17. Chen J, Li L, Huang G, et al. Numerical investigations of ducted fan aerodynamic performance with tip-jet. Aerospace Sci Tech, 2018, 78: 510–521

    Article  Google Scholar 

  18. Misiorowski M, Gandhi F, Oberai A A. A computational study on diffuser length variation for a ducted rotor in hover and edgewise flight. In: Proceedings of the American Helicopter Society Aeromechanics Specialists Meeting. San Francisco, 2018

  19. Qing J X, Hu Y, Wang Y L, et al. Kriging assisted integrated rotorduct optimization for ducted fan in hover. In: Proceedings of the AIAA Scitech 2019 Forum. San Diego, 2019. 7

  20. Fan C, Amankwa Adjei R, Wu Y, et al. Parametric study on the aerodynamic performance of a ducted-fan rotor using free-form method. Aerospace Sci Tech, 2020, 101: 105842

    Article  Google Scholar 

  21. Kim W Y, Senguttuvan S, Kim S M. Effect of rotor spacing and duct diffusion angle on the aerodynamic performances of a counter-rotating ducted fan in hover mode. Processes, 2020, 8: 1338

    Article  Google Scholar 

  22. Lee S W, Kim J K. Numerical investigation on the hovering performance of contra-rotating ducted rotor for micro air vehicle. Microsyst Technol, 2020, 26: 3569–3580

    Article  Google Scholar 

  23. Cao C, Zhao G, Zhao Q, et al. Numerical investigation and optimization for interior duct shape of ducted tail rotor. Aerospace Sci Tech, 2021, 115: 106778

    Article  Google Scholar 

  24. Zhang T, Barakos G N. High-fidelity numerical analysis and optimisation of ducted propeller aerodynamics and acoustics. Aerospace Sci Tech, 2021, 113: 106708

    Article  Google Scholar 

  25. Zhang T, Qiao G, Smith D A, et al. Parametric study of aerodynamic performance of equivalent ducted/un-ducted rotors. Aerospace Sci Tech, 2021, 117: 106984

    Article  Google Scholar 

  26. Zhu C, Hu Z, Cai Z, et al. Numerical investigation on the influence of geometrical parameters on the aerodynamic performance of a small-scale ducted fans system. Arab J Sci Eng, 2021, 46: 11963–11970

    Article  Google Scholar 

  27. Camci C, Aktürk A. A VTOL-UAV inlet flow distortion reducition concept using a new flow control approach: Double-ducted-fan. In: Proceedings of the 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery. Hawaii, 2016

  28. Camci C, Herwig N, Aktürk A. Inlet flow separation control via novel lip-spoilers for ducted fan based VTOL uninhabited aerial vehicles. In: Proceedings of the 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery. Hawaii, 2016

  29. Ryu M, Cho L, Cho J. Aerodynamic analysis of the ducted fan for a VTOL UAV in crosswinds. Trans Jpn Soc Aero S Sci, 2016, 59: 47–55

    Article  Google Scholar 

  30. Deng S, Wang S, Zhang Z. Aerodynamic performance assessment of a ducted fan UAV for VTOL applications. Aerospace Sci Tech, 2020, 103: 105895

    Article  Google Scholar 

  31. Wang H T, Wang Y G, Deng S H. Experimental study of in-ground-effect on force and spectrum characteristics of a contra-rotating lift fan (in Chinese). J Propul Tech, 2018, 39: 69–75

    Google Scholar 

  32. Han H, Xiang C L, Xu B. Aerodynamic performance of shrouded coaxial anti-rotating rotor propulsion unit with ground effect (in Chinese). J Aerospace Power, 2019, 34: 39–48.

    Google Scholar 

  33. Ai T, Xu B, Xiang C, et al. Aerodynamic analysis and control for a novel coaxial ducted fan aerial robot in ground effect. Int J Adv Robotic Syst, 2020, 17: 172988142095302

    Article  Google Scholar 

  34. Jin Y, Fu Y, Qian Y, et al. A moore-greitzer model for ducted fans in ground effect. J Appl Fluid Mech, 2020, 13: 693–701

    Article  Google Scholar 

  35. Ai T, Xu B, Xiang C, et al. Modeling of a novel coaxial ducted fan aerial robot combined with corner environment by using artificial neural network. Sensors, 2020, 20: 5805

    Article  Google Scholar 

  36. Ai T, Fan W, Xu B, et al. Aerodynamic analysis and modeling of coaxial ducted fan aircraft with the ceiling effect. Eng Appl Comput Fluid Mech, 2021, 15: 1563–1584

    Google Scholar 

  37. Han H, Xiang C, Xu B, et al. Experimental and computational investigation on comparison of micro-scale open rotor and shrouded rotor hovering in ground effect. Proc Inst Mech Engineers Part G-J Aerospace Eng, 2021, 235: 553–565

    Article  Google Scholar 

  38. Sheng C, Zhao Q, Bi N P. Numerical investigations of ducted fan hover performance for FIW applications. In: Proceedings of the 53rd AIAA Aerospace Sciences Meeting. Kissimmee, 2015. 1935

  39. Akturk A, Camci C. Tip clearance investigation of a ducted fan used in VTOL UAVS: Part 1—baseline experiments and computational validation. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2011, 54679: 331–344

    Google Scholar 

  40. Hrishikeshavan V, Black J, Chopra I. Design and testing of a quad shrouded rotor micro air vehicle in hover. In: Proceedings of the 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 20th AIAA/ASME/AHS Adaptive Structures Conference 14th AIAA. 2012. 1720

  41. Akturk A, Camci C. Influence of tip clearance and inlet flow distortion on ducted fan performance in VTOL UAVs. In: Proceedings of the AHS Forum. Phoenix, 2010, 338. 111–121

  42. Leishman G J. Principles of Helicopter Aerodynamics. Cambridge: Cambridge University Press, 2006

    Google Scholar 

  43. Seddon J M, Newman S. Basic Helicopter Aerodynamics. New York: John Wiley & Sons, 2001

    Google Scholar 

  44. Hrishikeshavan V. Experimental investigation of a shrouded rotor micro air vehicle in hover and in edgewise gusts. Dissertation for Dcotoral Degree. College Park: University of Maryland, 2011

    Google Scholar 

  45. Park M J, Jang J S, Lee D J. Design, performance evaluation and contribution of each component of ducted fan UAV in hover. In: Proceedings of the 2nd Asian/Australian Rotorcraft Forum and the 4th International Basic Research Conference on Rotorcraft Technology. ARF International Executive Committee, 2013. 96–104

  46. Vilaça J, Vale A, Cunha F. Design optimization of a ducted-drone to perform inspection operations. In: Procedings of the Iberian Robotics Conference. Cham: Springer, 2019. 3–15

    Google Scholar 

  47. Jimenez B G, Singh R. Effect of duct-rotor aerodynamic interactions on blade design for hover and axial flight. In: Proceedings of the 53rd AIAA Aerospace Sciences Meeting. Kissimmee, 2015. 1030

  48. Yilmaz S, Erdem D, Kavsaoglu M. Effects of duct shape on a ducted propeller performance. In: Proceedings of the 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Grapevine, 2013. 803

  49. Wolf S, Johnston J P. Effects of nonuniform inlet velocity profiles on flow regimes and performance in two-dimensional diffusers. ASME J Basic Eng, 1969, 91: 462–474

    Article  Google Scholar 

  50. Platt Jr R J. Static tests of a shrouded and an unshrouded propeller. NASA Technical Reports Server, 1948

  51. Taylor R T. Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing. NASA Technical Reports Server, 1958

  52. Misiorowski M P, Gandhi F S, Oberai A A. Computational study of diffuser length on ducted rotor performance in edgewise flight. AIAA J, 2019, 57: 796–808

    Article  Google Scholar 

  53. Jiang Y, Zhang B. Numerical investigation of effect of parameters on hovering efficiency of an annular lift fan aircraft. Aerospace, 2016, 3: 35

    Article  Google Scholar 

  54. Mao Z, Tian W, Yan S. Influence analysis of blade chord length on the performance of a four-bladed Wollongong wind turbine. J Renew Sustain Energy, 2016, 8: 023303

    Article  Google Scholar 

  55. Zhao Q Y, Sheng C H. Numerical investigation and validation for open rotor hover performance. In: Proceedings of the 33rd AIAA Applied Aerodynamics Conference. Dallas, 2015. 3014

  56. Han D, Yang K, Barakos G N. Extendable chord for improved helicopter rotor performance. Aerospace Sci Tech, 2018, 80: 445–451

    Article  Google Scholar 

  57. Graf W, Fleming J, Ng W. Improving ducted fan UAV aerodynamics in forward flight. In: Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno, 2008. 430

  58. Cai H M, Ma G L, Li Z X. Aerodynamic characteristics of a ducted fan system based on momentum source method. J Phys-Conf Ser, 2019, 1300: 012061

    Article  Google Scholar 

  59. Fleming J, Jones T, Ng W, et al. Improving control system effectiveness for ducted fan VTOL UAVs operating in crosswinds. In: Proceedings of the 2nd AIAA “Unmanned Unlimited” Conference and Workshop & Exhibit. San Diego, 2003. 6514

  60. Hrishikeshavan V, Chopra I. Aeromechanics and control of a shrouded rotor micro air vehicle in hover and in edgewise flow. J Am Helicopter Soc, 2011, 56: 1–14

    Article  Google Scholar 

  61. Hrishikeshavan V, Chopra I. Performance, flight testing of a shrouded rotor micro air vehicle in edgewise gusts. J Aircraft, 2012, 49: 193–205

    Article  Google Scholar 

  62. Hrishikeshavan V. Experimental investigation of a shrouded rotor micro air vehicle in hover and in edgewise gusts. College Park: University of Maryland, 2011

    Google Scholar 

  63. Hrishikeshavan V, Black J, Chopra I. Development of a quad shrouded rotor micro air vehicle and performance evaluation in edgewise flow. In: Proceedings of the American Helicopter Society Forum. Dallas, 2012

  64. Halwick J M. Implementation of blade element theory in CFD analysis of edgewise ducted fan vehicles. Dissertation for Master’s Degree. University Park: The Pennsylvania State University, 2012

    Google Scholar 

  65. Martin P, Tung C. Performance and flowfield measurements on a 10-inch ducted rotor vtol UAV. In: Proceedings of the 60th Annual Forum of the American Helicopter Society. American Helicopter Society, Alexandria, 2004

  66. Xu H Y, Xing S L, Ye Z Y. Numerical study of ducted-fan lip stall suppression based on inflatable leading lip cell. Procedia Eng, 2015, 126: 158–162

    Article  Google Scholar 

  67. Akturk A, Camci C. Lip separation and inlet flow distortion control in ducted fans used in VTOL systems. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2014, 45578: V01AT01A027

    Google Scholar 

  68. Matus-Vargas A, Rodriguez-Gomez G, Martinez-Carranza J. Ground effect on rotorcraft unmanned aerial vehicles: A review. Intel Serv Robotics, 2021, 14: 99–118

    Article  Google Scholar 

  69. Gallo M. Aviation accident final report. Fatal CEN11FA507, National Transportation Safety Board, 2013

  70. Rayner B. Aviation accident final report. Non-fatal ERA16CA160, National Transportation Safety Board, 2016

  71. Hosseini Z. Ground/wall effects on a ducted fan for control applications of highly manoeuvrable vtols operating in confined spaces. Dissertation for Dcotoral Degree. Calgary: University of Calgary, 2011

    Google Scholar 

  72. Norton D. Influence of ground effects on body forces for bi-copter UAV. Dissertation for Master’s Degree. Calgary: University of Calgary, 2017

    Google Scholar 

  73. Hosseini Z, Martinuzzi R J, Ramirez Serrano A. Analyzing the performance of a hovering ducted rotor in ground/wall effects to improve the controlling aspects of VTOL vehicles in confined spaces. In: Proceedings of the Fluids Engineering Division Summer Meeting. Montreal, 2010, 49484. 981–986

  74. Fan W, Xu B, Xiang C, et al. A novel approach to the attitude stabilization structure for ducted-fan operative aerial robots: Finding improvements for modeling error and strong external transient disturbance. Chin J Aeronaut, 2022, 35: 250–264

    Article  Google Scholar 

  75. Hosseini Z, Ramirez-Serrano A, Martinuzzi R J. Ground/wall effects on a tilting ducted fan. Int J Micro Air Vehicles, 2011, 3: 119–141

    Article  Google Scholar 

  76. Amitay M, Pitt D, Glezer A. Separation control in duct flows. J Aircraft, 2002, 39: 616–620

    Article  Google Scholar 

  77. Vukasinovic B, Brzozowski D, Glezer A. Fluidic control of separation over a hemispherical turret. AIAA J, 2009, 47: 2212–2222

    Article  Google Scholar 

  78. Li J. Self-adaptive stability-enhancing technology with tip air injection in an axial flow compressor. J TurboMach, 2017, 139: 011008

    Article  Google Scholar 

  79. Gilarranz J L, Traub L W, Rediniotis O K. A new class of synthetic jet actuators—part II: Application to flow separation control. J Fluids Eng, 2005, 127: 377–387

    Article  Google Scholar 

  80. Whitehead J, Gursul I. Interaction of synthetic jet propulsion with airfoil aerodynamics at low Reynolds numbers. AIAA J, 2006, 44: 1753–1766

    Article  Google Scholar 

  81. Pavlova A, Amitay M. Electronic cooling using synthetic jet impingement. ASME J Heat Transfer, 2006, 128: 897–907

    Article  Google Scholar 

  82. Ohanian O J. Ducted fan aerodynamics and modeling, with applications of steady and synthetic jet flow control. Virginia Tech, 2011

  83. Li L, Huang G P, Chen J. Effects of tip-jet on the performance of a ducted fan. Proc Inst Mech Eng Part G-J Aerospace Eng, 2020, 234: 508–521

    Article  Google Scholar 

  84. Li L, Huang G, Chen J. Aerodynamic characteristics of a tip-jet fan with a large blade pitch angle. Aerospace Sci Tech, 2019, 91: 49–58

    Article  Google Scholar 

  85. Camci C, Akturk A. Double ducted fan (DDF). The Pennsylvania State University, 2010

  86. Lanchester F W. Contra-props, recollections of early considerations by advisory committee for aeronautics a Pioneer’s 1907 patent, suggestions for further research. Flight, 1941

  87. Ye L, Xu G H. Calculation on flow field and aerodynamic force of coaxial rotors in hover with CFD method (in Chinese). Acta Aerodyn Sin, 2012, 30: 437–42.

    MathSciNet  Google Scholar 

  88. Cai H M, Zhang Z R, Deng S H. Numerical prediction of unsteady aerodynamics of a ducted fan unmanned aerial vehicle in hovering. Aerospace, 2022, 9: 318

    Article  Google Scholar 

  89. Mistry C, Pradeep A M. Influence of circumferential inflow distortion on the performance of a low speed, high aspect ratio contra rotating axial fan. J TurboMach, 2014, 136: 071009

    Article  Google Scholar 

  90. Akturk A, Camci C. Tip clearance investigation of a ducted fan used in VTOL unmanned aerial vehicles—Part II: Novel treatments via computational design and their experimental verification. J TurboMach, 2014, 136: 021004

    Article  Google Scholar 

  91. Colman M, Suzuki S, Kubo D. Wind tunnel test results and performance prediction for a ducted fan with collective and cyclic pitch actuation for VTOL with efficient cruise. In: Proceedings of the AIAA Atmospheric Flight Mechanics Conference. Portland, 2011. 6379

  92. Zhao J, Hou Q M, Jin H Z, et al. CFD analysis of ducted-fan UAV based on Magnus effect. In: Proceedings of the 2012 IEEE International Conference on Mechatronics and Automation. IEEE, 2012. 1722–1726

  93. Hou Q M, Zhu Y H, Zhao J, et al. A novel ducted-fan UAV model using magnus effect steering engine. J Aeronaut Astronaut Aviat, 2014, 46: 209–217

    Google Scholar 

  94. Boinov K O, Lomonova E A, Vandenput A J A, et al. Surge control of the electrically driven centrifugal compressor. IEEE Trans Ind Applicat, 2006, 42: 1523–1531

    Article  Google Scholar 

  95. Bianchi S, Corsini A, Mazzucco L, et al. Stall inception, evolution and control in a low speed axial fan with variable pitch in motion. J Eng Gas Turbines Power, 2012, 134: 042602

    Article  Google Scholar 

  96. Barbarino S, Gandhi F, Webster S D. Design of extendable chord sections for morphing helicopter rotor blades. J Intelligent Material Syst Struct, 2011, 22: 891–905

    Article  Google Scholar 

  97. Bianchi S, Corsini A, Sheard A G, et al. A critical review of stall control techniques in industrial fans. ISRN Mech Eng, 2013, 2013: 1–18

    Article  Google Scholar 

  98. Bianchi S, Corsini A, Sheard A G. Detection of stall regions in a low-speed axial fan: Part I—Azimuthal acoustic measurements. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2010, 43987: 169–179

    Google Scholar 

  99. Jia G W, Cai M L, Xu W Q, et al. Energy conversion characteristics of reciprocating piston quasi-isothermal compression systems using water sprays. Sci China Tech Sci, 2018, 61: 285–298

    Article  Google Scholar 

  100. Shi Y, Chang J Q, Wang Y X, et al. Gas leakage detection and pressure difference identification by asymmetric differential pressure method. Chin J Mechl Eng, 2022, 35: 1–10

    Google Scholar 

  101. Eichenberg D J, Solano P A, Thompson W K, et al. Development of a 32 inch diameter levitated ducted fan conceptual design. NASA Technical Reports Server, 2006

  102. Jin Y, Qian Y, Zhang Y, et al. Modeling of ducted-fan and motor in an electric aircraft and a preliminary integrated design. SAE Int J Aerosp, 2018, 11: 115–126

    Article  Google Scholar 

  103. Balachandran T, Reband J D, Xiao J, et al. Co-design of an integrated direct-drive electric motor and ducted propeller for aircraft propulsion. In: Proceedings of the 2020 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS). IEEE, 2020. 1–11

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Correspondence to YangJun Zhang.

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This work was supported by the National Key Research and Development Program of China (Grant No. 2020YFC1512500), the Advanced Aviation Power Innovation Institution, the Aero Engine Academy of China, and Tsinghua University Initiative Scientific Research Program.

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Qian, Y., Luo, Y., Hu, X. et al. Improving the performance of ducted fans for VTOL applications: A review. Sci. China Technol. Sci. 65, 2521–2541 (2022). https://doi.org/10.1007/s11431-021-2110-x

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