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Review on ducted fans for compound rotorcraft

Part of: 75 year anniversary of Aeronautical Engineering at Glasgow University

Published online by Cambridge University Press:  16 January 2020

T. Zhang  and
G.N. Barakos Open the ORCID record for G.N. Barakos [Opens in a new window]
T. Zhang
Affiliation:
CFD Laboratory, School of Engineering University of GlasgowGlasgowUK
G.N. Barakos*
Affiliation:
CFD Laboratory, School of Engineering University of GlasgowGlasgowUK
*
george.barakos@glasgow.ac.uk
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Abstract

This paper presents a survey of published works on ducted fans for aeronautical applications. Early and recent experiments on full- or model-scale ducted fans are reviewed. Theoretical studies, lower-order simulations and high-fidelity CFD simulations are also summarised. Test matrices of several experimental and numerical studies are compiled and discussed. The paper closes with a summary of challenges for future ducted fan research.

Keywords

Ducted rotorDucted fanPropulsor
Type
Survey Papers
Information
The Aeronautical Journal , Volume 124 , Issue 1277 , July 2020 , pp. 941 - 974
Copyright
© Royal Aeronautical Society 2020

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References

Stipa, L. Experiments with intubed propellers, NACA Technical Memorandum 655, Washington DC, 1932.Google Scholar
Sacks, A. and Burnell, J.Ducted propellers: a critical review of the state of the art, Prog Aeronaut Sci, 1962, 3, pp 85–135.CrossRefGoogle Scholar
Pereira, J.L. Hover and Wind-Tunnel Testing of Shrouded Rotors for Improved Micro Air Vehicle Design, Ph.D. thesis, 2008.Google Scholar
Akturk, A. and Camci, C. Double Ducted Fan (DDF) as a novel ducted fan inlet lip separation control device, The International Powered Lift Conference, October 2010, pp 148–170.Google Scholar
Fletcher, H.S. Experimental investigation of lift, drag, and pitching moment of five annular airfoils, Tech Rep, NACA-TN-4117, 1957.Google Scholar
Krüger, W. On wind tunnel tests and computations concerning the problem of shrouded propellers, Tech Rep, National Advisory Committee for Aeronautics, 1949.Google Scholar
Platt, R.J. Static tests of a shrouded and an unshrouded propeller, Tech Rep, National Advisory Committee for Aeronautics, 1948.Google Scholar
Grunwald, K.J. and Goodson, K.W. Aerodynamic loads on an isolated shrouded-propeller configuration for angles of attack from –10 degrees to 110 degrees, Tech Rep, National Aeronautics and Space Administration Washington DC, 1962.Google Scholar
Carlton, J.Marine Propellers and Propulsion, 4th ed, London, Butterworth-Heinemann, 2018.CrossRefGoogle Scholar
Gilbert, B., Oman, R. and Foreman, K.Fluid dynamics of diffuser-augmented wind turbines, J. Energy, 1978, 2, (6), pp 368–374.CrossRefGoogle Scholar
Ohya, Y., Karasudani, T., Sakurai, A., Abe, K.-i. and Inoue, M.Development of a shrouded wind turbine with a flanged diffuser, J Wind Eng Ind Aerodyn, 2008, 96, (5), pp 524–539.CrossRefGoogle Scholar
Gaffey, T.M., Zhang, C., Quackenbush, T.R., Sheng, C. and Hasbun, M. Aeromechanics of the coaxial compound helicopter, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2015.Google Scholar
Johnson, W., Elmore, J., Keen, E., Gallaher, A. and Nunez, G. Coaxial compound helicopter for confined urban operations, 2016, pp 210–239.Google Scholar
Goodson, K.W. and Grunwald, K.J. Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight, Tech Rep, NASA TN D-981, 1962.Google Scholar
Hubbard, H.H. Sound measurements for five shrouded propellers at static conditions, Tech Rep, National Advisory Committee for Aeronautics, 1950.Google Scholar
Parlett, L.P. Aerodynamic characteristics of a small-scale shrouded propeller at angles of attack from 0 to 90 degrees, Tech Rep, NACA-TN-3547, 1955.Google Scholar
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, Tech Rep, National Advisory Committee for Aeronautics, 1958.Google Scholar
Yaggy, P.F. and Mort, K.W. A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing, Tech Rep, NASA-TN-D-776, 1961.Google Scholar
Grunwald, K.J. and Goodson, K.W. Division of aerodynamic loads on a semispan tilting-ducted-propeller model in hovering and transition flight, Tech Rep, NASA TN D-1257, 1962.Google Scholar
Mort, K.W. and Gamse, B. A wind-tunnel investigation of a 7-foot-diameter ducted propeller, Tech Rep, NASA-TN-D-4142, 1967.Google Scholar
Black, D. and Rohrbach, C. Shrouded propellers-a comprehensive performance study, 5th Annual Meeting and Technical Display, 1968, p 994.CrossRefGoogle Scholar
Mort, K.W. and Yaggy, P.F. Aerodynamic characteristics of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing, Tech Rep, NASA-TN-D-1301, 1962.Google Scholar
Mort, K.W. Performance characteristics of a 4-foot-diameter ducted fan at zero angle of attack for several fan blade angles, Tech Rep, NASA-TN-D-3122, 1966.Google Scholar
Yaggy, P.F. and Goodson, K.W. Aerodynamics of tilting ducted-fan configurations, Tech Rep, NASA Langley Research Center, 1961.Google Scholar
Kriebel, A.R. and Mendenhall, M.R. Predicted and measured performance of two full-scale ducted propellers, Tech Rep, NASA-CR-578, 1966.Google Scholar
Bahram, R. Aerodynamic Study of Tilting Asymmetrical Ducted Fans Mounted at the Wing Tips of a VTOL UAV, PhD thesis, 2016.Google Scholar
Xu, H.-Y., Xing, S.-L. and Ye, Z.-Y.Numerical study of ducted-fan lip stall suppression based on inflatable leading lip cell, Procedia Eng, 2015, 126, pp 158–162.CrossRefGoogle Scholar
Abrego, A.I., Bulaga, R.W. and Rutkowski, M. Performance study of a ducted fan system, The American Helicopter Society Aerodynamics, Acoustics, and Test and Evaluation Technical Specialists Meeting, San Francisco, CA, 2002.Google Scholar
Fleming, J., Jones, T., Ng, W., Gelhausen, P. and Enns, D. Improving control system effectiveness for ducted fan VTOL UAVs operating in crosswinds, 2nd AIAA Unmanned Unlimited Conf. and Workshop & Exhibit, 2003, p 6514.CrossRefGoogle Scholar
Martin, P. and Tung, C. Performance and flowfield measurements on a 10-inch ducted rotor vtol uav, Tech Rep, Army Research Development and Engineering Command, Moffett Field CA, Aviation Aeroflight Dynamics Directorate, 2004.Google Scholar
Graf, W., Fleming, J. and Ng, W. Improving ducted fan UAV aerodynamics in forward flight, 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008, p 430.CrossRefGoogle Scholar
Akturk, A., Shavalikul, A. and Camci, C. PIV measurements and computational study of a 5-inch ducted fan for V/STOL UAV applications, 47th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, Florida, 2009, p 332.CrossRefGoogle Scholar
Ohanian, O., Gelhausen, P. and Inman, D. A compact method for modeling the aerodynamics of ducted fan vehicles, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2010, p 1052.CrossRefGoogle Scholar
Akturk, A. and Camci, C. Tip clearance investigation of a ducted fan used in VTOL UAVS: part 1: baseline experiments and computational validation, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, American Society of Mechanical Engineers, 2011, pp 331–344.CrossRefGoogle Scholar
Rhee, W., Myers, L. and McLaughlin, D. Aeroacoustics of vertical lift ducted rotors, 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2013, p 3333.Google Scholar
Yilmaz, S., Erdem, D. and Kavsaoglu, M. Effects of duct shape on a ducted propeller performance, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013, p 803.CrossRefGoogle Scholar
Chang, I.-C. and Rajagopalan, R. CFD analysis for ducted fans with validation, 21st AIAA Applied Aerodynamics Conference, 2003, p 4079.CrossRefGoogle Scholar
Lind, R., Nathman, J. and Gilchrist, I. Ducted rotor performance calculations and comparison with experimental data, 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006, p 1069.CrossRefGoogle Scholar
Camci, C. and Akturk, A. Double-ducted fan, 2014, US Patent 8,821,123.Google Scholar
Akturk, A. and Camci, C.Experimental and computational assessment of a ducted-fan rotor flow model, J Aircr, 2012, 49, (3), pp 885–897.CrossRefGoogle Scholar
Akturk, A. and Camci, C. Tip clearance investigation of a ducted fan used in VTOL UAVS: part 2: novel treatments via computational design and their experimental verification, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, American Society of Mechanical Engineers, 2011, pp 345–357.CrossRefGoogle Scholar
Thwaites, B. A note on the design of ducted fans, Aeronaut Q, 1951, 3, (3), pp 173–181.CrossRefGoogle Scholar
Thwaites, B. A note on the performance of ducted fans, Aeronaut Q, 1953, 4, (2), pp 179–185.CrossRefGoogle Scholar
Bontempo, R. and Manna, M.Solution of the flow over a non-uniform heavily loaded ducted actuator disk, J Fluid Mech, 2013, 728, pp 163–195.CrossRefGoogle Scholar
Bontempo, R. and Manna, M. Effects of duct cross section camber and thickness on the performance of ducted propulsion systems for aeronautical applications, Int J Aerosp Eng, 2016, 2016, pp 9. doi: 10.1155/2016/8913901CrossRefGoogle Scholar
Youngren, H., Drela, M. and Sanders, S. Ducted fan design code, http://web.mit.edu/drela/Public/web/dfdc/, December 2005.Google Scholar
Bi, N., Kimmel, K. and Haas, D.J. Performance investigation of ducted aerodynamic propulsors, First International Symposium on Marine Propulsors, Smp, Vol. 9, 2009.Google Scholar
Ko, A., Ohanian, O. and Gelhausen, P. Ducted fan UAV modeling and simulation in preliminary design, AIAA Modeling and Simulation Technologies Conference and Exhibit, 2007, p 6375.CrossRefGoogle Scholar
Ahn, J. and Lee, K. Performance prediction and design of a ducted fan system, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, p 4196.Google Scholar
Ahn, J. and Drela, M. Newton method on axisymmetric transonic flow and linearized 3D flow prediction, 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998, p 928.CrossRefGoogle Scholar
Drela, M. and Youngre, H. Axisymmetric analysis and design of ducted rotors, http://web.mit.edu/drela/Public/web/dfdc/DFDCtheory12-31.pdf, December 2005.Google Scholar
Guerrero, I., Londenberg, W.K., Gelhausen, P. and Myklebust, A. A powered lift aerodynamic analysis for the design of ducted fan UAVs, 2nd AIAA Unmanned Unlimited Conference and Workshop & Exhibit, 2003, p 6567.CrossRefGoogle Scholar
Rajagopalan, R. and Zhang, Z. Performance and flow field of a ducted propeller, 25th Joint Propulsion Conference, 1989, p 2673.CrossRefGoogle Scholar
Ye, K., Ye, Z.-Y. and Qu, Z.Aerodynamic optimization method for duct design, J Aerosp Power, 28, 08 2013, pp 1828–1835.Google Scholar
Sheng, C., Zhao, Q. and Bi, N.P. Numerical investigations of ducted fan hover performance for FIW applications, 53rd AIAA Aerospace Sciences Meeting, 2015, p. 1935.CrossRefGoogle Scholar
Jimenez, B.G. and Singh, R. Effect of duct-rotor aerodynamic interactions on blade design for hover and axial flight, 53rd AIAA Aerospace Sciences Meeting, 2015, p 1030.CrossRefGoogle Scholar
Biava, M. and Barakos, G.N.Optimisation of ducted propellers for hybrid air vehicles using high-fidelity CFD, Aeronaut J, 2016, 120, (1232), pp 1632–1657.CrossRefGoogle Scholar
Chen, J., Li, L., Huang, G. and Xiang, X.Numerical investigations of ducted fan aerodynamic performance with tip-jet, Aerosp Sci Technol, 2018, 78, pp 510–521.CrossRefGoogle Scholar
Rubio, R.C., Diaz, P.V. and Yoon, S. High-fidelity computational analysis of ducted and coaxial rotors for urban air mobility, Proceedings of the 75th Annual Forum, Philadelphia, May 2019.Google Scholar
Singh, R., Jimenez, B. and Avera, M. Investigation of aerodynamic interactions in ducted rotor systems, The AHS 70th Annual Forum, 2014.Google Scholar
Li, L., Huang, G., Chen, J. and Yuan, J. Numerical experiment of tip-jet ducted fans with various nozzles, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, p 5093.CrossRefGoogle Scholar
Schaller, D.F. A Technique for Shape Optimization of Ducted Fans, Master’s thesis, Iowa State University, 2007.Google Scholar
Qing, J., Hu, Y., Wang, Y., Liu, Z., Fu, X. and Liu, W. Kriging assisted integrated rotor-duct optimization for ducted fan in Hover, AIAA Scitech 2019 Forum, 2019, p 0007.CrossRefGoogle Scholar
Rajagopalan, R.G. and Mathur, S.R.Three dimensional analysis of a rotor in forward flight, J Am Helicopter Soc, 1993, 38, (3), pp 14–25.CrossRefGoogle Scholar
Myers, L.M. Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight, Master’s thesis, 2009.Google Scholar
Ohanian, O.J., Karni, E.D., Londenberg, W.K., Gelhausen, P.A. and Inman, D.J.Ducted-fan force and moment control via steady and synthetic jets, J Aircr, 2011, 48, (2), pp 514–526.CrossRefGoogle Scholar
Kondor, S.A. and Moore, M. Experimental investigation of a morphing nacelle ducted fan (NASA/CP-2005-213509), 2004 NASA/ONR Circulation Control Workshop, 16–17 March 2004, 2004, pp 435–468.Google Scholar
Colman, M., Suzuki, S., and Kubo, D. Wind tunnel test results and performance prediction for a ducted fan with collective and cyclic pitch actuation for VTOL with efficient cruise, AIAA Atmospheric Flight Mechanics Conference, 2011, p 6379.CrossRefGoogle Scholar
Gilmore, A. and Grahame, W.Research studies on a ducted fan equipped with turning vanes, J Am Helicopter Soc, 1959, 4, (4), pp 11–21.CrossRefGoogle Scholar
Oweis, G.F., Fry, D., Chesnakas, C.J., Jessup, S.D. and Ceccio, S.L.Development of a tip-leakage flow - part 1: the flow over a range of Reynolds numbers, J Fluids Eng, 2006, 128, (4), pp 751–764.CrossRefGoogle Scholar
Oweis, G.F., Fry, D., Chesnakas, C.J., Jessup, S.D. and Ceccio, S.L.Development of a tip-leakage flow - part 2: comparison between the ducted and un-ducted rotor, J Fluids Eng, 2006, 128, (4), pp 765–773.CrossRefGoogle Scholar
Martin, P. and Boxwell, D. Design, analysis and experiments on a 10-inch ducted rotor VTOL UAV, American Helicopter Society (AHS) International Specialists Meeting on Unmanned Rotorcraft: Design, Control and Testing, Chandler, AZ, January, 2005, pp 18–20.Google Scholar
Ryu, M., Cho, L. and Cho, J.The effect of tip clearance on performance of a counter-rotating ducted fan in a VTOL UAV, Japan Society, 2017, 60, (1), pp 1–9.Google Scholar
Rumsey, C.L., Biedron, R., Farassat, F. and Spence, P.Ducted-fan engine acoustic predictions using a Navier–Stokes code, J Sound Vib, 1998, 213, (4), pp 643–664.CrossRefGoogle Scholar
Nark, D., Farassat, F., Pope, D.S. and Vatsa, V. The development of the ducted fan noise propagation and radiation code CDUCT-LARC, 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003, p 3242.CrossRefGoogle Scholar
Reboul, G., Polacsek, C., Lewy, S. and Heib, S.Aeroacoustic computation of ducted-fan broadband noise using LES data, J Acoust Soc Am, 2008, 123, (5), pp 3539–3539.CrossRefGoogle Scholar
Shur, M., Strelets, M., Travin, A., Christophe, J., Kucukcoskun, K., Schram, C.F., Sack, S. and Åbom, M. Effect of inlet distortions on ducted fan noise, 22nd AIAA/CEAS Aeroacoustics Conference, 2016, p 2819.CrossRefGoogle Scholar
Eversman, W. Theoretical models for duct acoustic propagation and radiation, 1991.Google Scholar
Groeneweg, J.F., Sofrin, T., Rice, E. and P.R., G. Aeroacoustics of Flight Vehicles: Theory and Practice, Vol 1: Turbomachinery noise, chap. 3, NASA Rep 1258, 1991, pp. 151–210.Google Scholar
Motsinger, R. and Kraft, R. Design and performance of duct acoustic treatment, In: Aeroacoustics of Flight Vehicles: Theory and Practice, Vol. 2, Chap. 14, NASA Rep 1258, 1991, pp. 165–206.Google Scholar
Astley, R., Sugimoto, R., Achunche, I., Kewin, M., Mustafi, P. and Deane, E. A review of CAA for fan duct propagation and radiation, with application to liner optimisation, Procedia Engineering, Vol. 6, 2010, pp 143–152.CrossRefGoogle Scholar
Tyler, J.M. and Sofrin, T.G. Axial flow compressor noise studies, Tech Rep, SAE Technical Paper, 1962.CrossRefGoogle Scholar
Dunn, M., Tweed, J. and Farassat, F.The application of a boundary integral equation method to the prediction of ducted fan engine noise, J Sound Vib, 1999, 227, (5), pp 1019–1048.CrossRefGoogle Scholar
Dunn, M.H. TBIEM3D: a computer program for predicting ducted fan engine noise. Version 1.1, Tech Rep, NASA/CR-97-206232, 1997.Google Scholar
Wang, T., Yang, B. and Guan, Y. A study on the prediction of the ducted fan noise, 11th AIAA/CEAS Aeroacoustics Conference, 2005, p 3069.CrossRefGoogle Scholar
Choi, H.L., Jeon, W. and Lee, D.-J. Duct effects on aeroacoustic noise of an axial fan, ICA 2004, Acoustical Society of Japan, 2004, pp 3261–3264.Google Scholar
Bulaga, R. Ducted fan efficiency and noise, Aerospace Technology Conference and Exposition, 2005.CrossRefGoogle Scholar
Malgoezar, A.M., Vieira, A., Snellen, M., Simons, D.G. and Veldhuis, L.L. Experimental characterization of noise radiation from a ducted propeller of an unmanned aerial vehicle, Int J Aeroacoust, 2019.CrossRefGoogle Scholar
Zhao, J., Hou, Q., Jin, H., Zhu, Y. and Li, G. CFD analysis of ducted-fan UAV based on magnus effect, 2012 IEEE International Conference on Mechatronics and Automation, IEEE, 2012, pp 1722–1726.CrossRefGoogle Scholar
Hou, Q.-M., Zhu, Y.-H., Zhao, J., Li, G. and Jin, H.-Z.A novel ducted-fan UAV model using magnus effect steering engine, J Aeronaut Astronaut Aviat, 2014, 46, (3), pp 209–217.Google Scholar
Lee, T.E. Design and Performance of a Ducted Coaxial Rotor in Hover and Forward Flight, Master’s thesis, University of Maryland.Google Scholar
Geldenhuys, H.J. Aerodynamic Development of a Contra-Rotating Shrouded Rotor System for a UAV, Master’s thesis, Stellenbosch University.Google Scholar
Jiang, Y., Li, H. and Jia, H. Aerodynamics optimization of a ducted coaxial rotor in forward flight using orthogonal test design, Shock and Vibration, 2018, 2018, pp 9. doi: 10.1155/2018/2670439CrossRefGoogle Scholar
Nemnem, A.F., Zakaria, M.Y. and Elzahaby, A.M. Contra-rotating ducted fan aerothermodynamic design procedure for unmanned applications, 2018 AIAA Information Systems-AIAA Infotech@ Aerospace, 2018, p 0745.CrossRefGoogle Scholar