Bibliography

 
 

Being fundamental to the State of the Art, major publications related to each Technology Stream have been gathered hereunder. The list includes the publications generated by the consortium since the project start:



HLFC technology applied on fin and wing (TS1)

  • Outputs from AFloNext
  • P. Wong, S. Walters, “Design and Performance Analysis of a Hybrid Laminar Flow Control (HLFC) Concept for a Civil Transport Aircraft”, Greener Aviation Conference 2016, 11-13 October 2016

  • Dirk M. Franke and Jochen Wild;” Aerodynamic Design of a Folded Krueger Device for a HLFC Wing”, STAB Symposium 2014, 4-5 November 2014


  • General references
  • E. Torenbeek: "Synthesis of Subsonic Airplane Design". Kluwer Academic Publishers, Dordrecht/Boston/London, 1982
  • D. W. Bechert et al.: "Experiments on drag-reducing surfaces and their optimization with an adjustable geometry". Journal of Fluid Mechanics (1997), Vol. 338, pp. 59-87, 1997
  • G. Schrauf: "Status and perspectives of laminar flow". The Aeronautical Journal, December 2005, Volume 109, Number 1102, pp. 639-644
  • R. D. Joslin: "Overview of Laminar Flow Control". NASA/TP-1998-208705, October 1998
  • R.Henke. "A320 HLF Fin Flight Tests Completed". Air&Space Europe, Vol 1, No.2, 1999, 76-79
  • G. Schrauf, K H. Horstmann: Simplified Hybrid Laminar Flow Control. ECCOMAS 2004, Jyväskylä, Finland, 24-28 July 2004, CD-Proceedings Volume II
  • G. Schrauf, H. von Geyr: "Simplified Hybrid Laminar Flow Control for Transport Aircraft". CD-ROM Proceedings of the 6th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2012), September 10-14, 2012, Vienna, Austria, ISBN: 978-3-9502481-9-7
  • W. E. Gray: The Effect of Wing Sweep on Laminar Flow". Royal Aircraft Establishment, Farnborough, February 1952
  • M. Gerber: "Grenzschichtabsaugung ohne Pumpe". Diplomarbeit, Technische Universität Dresden, 2009
  • M. Mecham: "First articles - 787-9 laminar flow studies validated as Boeing completes first fuselage articles". Aviation Week & Space Technology, 9 April 2012, p. 42
  • Boeing B787-8 with HLFC VTP: http://www.flightglobal.com/blogs/flightblogger/2011/06/photo-of-note-boeing-tests-hyb.html

Flow control technologies applied on outer wing (TS2)

  • Outputs from AFloNext
  • I. Detinis, M. Steinbuch, S. Segal, M. Lagutin, A. Seifert, M. Wasserman, Y. Levi, “Active Flow Control Implementation for Mitigating Outer Wing Flow Separation”, IACAS 2017, 15-16 March 2017
  • J.P. Rosenblum, P. Vrchota, S. Wallin, P. Eliasson, P. Iannelli, V. Ciobaca, J. Wild, J.L. Hantrais-Gervois, M. Costes, “Numerical sizing of Active Flow Control concepts on the outer wing”, 3AF International Conference on Applied Aerodynamics 2017, 27-29 March 2017
  • D. Dolgopyat, A. Seifert, “Conventional Airfoil Active Flow Control “Virtual” Maneuvering System", IACAS 2015, 25-26 February 2015

  • General references
  • A. Jameson et al., "Aerodynamic Simulation and Shape Optimization for High Speed Flow", 44th Aerospace Sciences Meeting, Reno, NV, January 9-12, 2006
  • I. Kroo, "Drag Due to Lift: Concepts for Prediction and Reduction", Annual Review of Fluid Mechanics, Vol. 33, pp. 587-617, 2001
  • J.-J. Chattot, "Analysis and Design of Wings and Wing/Winglet Combinations at Low Speeds", AIAA Paper 2004-0220, Jan. 2004
  • J. M. Kuhlman, M. J. Cerney, P. Liaw, "Transonic Low Aspect Ratio Wing-Winglet Design", AIAA Paper 88-0007, Jan. 1988

Technologies for local flow separation control applied in wing/pylon junction (TS3)

  • Outputs from AFloNext
  • P. Schloesser, M. Meyer, M. Schueller, P. Weigel, M. Bauer, “Fluidic Actuators ForSeparation Control At The Engine/Wing Junction”, Aircraft Engineering and Aerospace Technology Journal
  • P. Schloesser, M. Meyer, “Active Separation Control At The Engine/Wing Junction By Pulsed Excitation”, AIAA Aviation 2017, 5-9 June 2017

  • P. Vrchota, A. Prachař, P. Hospodář, D. Dolgopyat, A. Seifert, “Development of Simplified Boundary Condition of SaOB Actuator Based on High-Fidelity CFD Simulations”, 3AF International Conference on Applied Aerodynamics 2017, 27-29 March 2017

  • P. Vrchota, A. Prachar, „ Active Flow Separation Control Applied at Wing-Pylon Junction of a Wing Section in Landing Configuration”, AIAA SciTech 2017, 9-13 January 2017

  • P. Schloesser, M. Meyer, M. Schueller, P. Weigel, M. Bauer, “Optimization And Testing Of Fluidic Actuators For Active Flow Control At The Engine/Wing Junction”, EASN 2016, 18-21 October 2016

  • P. Vrchota, “Application Of Synthetic Jets Actuators In Wing-Pylon Junction Area To Improve The High Lift Performances”, ECCOMAS 2016, 5-10 June 2016

  • M. Meyer, “Design and Validation of Active Flow Separation Control at the Wing/Engine Junction”, ECCOMAS 2016, 5-10 June 2016

  • M. Schueller, P. Weigel, M. Lipowski, M. Meyer, P. Schlösser, M. Bauer, “Fluidic Actuators for Active Flow Control on Airframe”, SPIE Smart Structures 2016, 20-24 March 2016

  • A. Kröhnert, S. Fricke, M. Meyer, P. Schlösser, W. Machunze, M. Bauer, “Aerodynamic Design at the DLR Institute of Aerodynamics and Flow Technology as Crucial Enabler for Realizing Flow Control at the Engine/Wing Pylon”, Special edition of the book (Springer series) with the proceedings of the DLR-Symposium "High-Lift System Research - celebrating 10 years of DLR-F15", December 2015

  • J. Alderman, M. Meyer, M. Bottemanne, C. Atkin, A. Mann, “Future wing Hybrid Laminar Flow Control suction system design and analysis”, CEAS 2015, 7-11 September 2015

  • S. Fricke, V. Ciobaca, A. Kröhnert, J. Wild, O. Blesbois, “Active Flow Control Applied at the Engine-Wing Junction”, CEAS 2015, 7-11 September 2015

  • S. Fricke, V. Ciobaca, “Studies of Active Flow Control for Suppression of Flow Separation Caused by UHBR Engine Integration”, Symposium “Simulation of Wing and Nacelle Stall”, 1-2 December 2014

  • M.Meyer, M. Lengers, H. Bieler, S. Fricke, J. Wild, and D. Norman; “ Designing and Testing Active Flow Control Systems at the Junction of Ultra-High Bypass Ratio Engines and the Wing”; WCCM XI, ECCM V, EFCD VI, 20-25 July 2014
  • S. Fricke, V. Ciobaca, J. Wild and D. Norman;” Numerical Studies of Active Flow Control applied at the Engine-Wing Junction”, FOR1066 Symposium, 22-23 June 2012

  • General references
  • M. D. Guynn et al.: "Refined Exploration of Turbofan Design Options for an Advanced Single-Aisle Transport". NASA/TM–2011-216883, 2011
  • A. B. Haines: "Scale Effects at High Lift and Low Speeds". AGARD-AG-323 Scale Effects on Aircraft and Weapon Aerodynamics edited by Young, A. D., pp. 27 – 65, 1999
  • P. May: "Aircraft airfoil with close-mounted engine and leading edge high lift system". Patent number 6364254, 2000
  • P. Meredith: "Viscous phenomena affecting high lift systems and suggestions for future CFD development". AGARD-CP-515 High Lift System Aerodynamics, pp. 19-1 – 19-8, 1993
  • R. Rudnik: "Stall Behaviour of the EUROLIFT High Lift Configurations". AIAA Paper 08-0836, 2008
  • P. Rudolf: "High-Lift Systems on Commercial Subsonic Airliners". NASA Contractor Report 4746, 1996
  • J.-C. Courty, T. DeLille: "Validation of in-tunnel High Lift Computations". Proceedings of European Air and Space Conference (CEAS 2007), Berlin, Germany, September 2007
  • H. Frh. V. Geyr et al.: "CFD Prediction of the Maximum Lift Effects on Realistic High LiftCommercial Aircraft Configurations within the European project EUROLIFT II". AIAA-2007-4299, 2007
  • F. Moens, J. Perraud: "Transition Prediction and Impact on 3D High-Lift Wing Configuration". AIAA-2007-4302, 2007
  • K.-P. Neitzke, R. Rudnik, A. Schröder: "Low Speed Validation Tests on Engine/Airframe". AIAA Paper 2005-3704, 2005
  • J. Perraud, F Moens: "Transport aircraft 3D high lift wing numerical transition prediction". AIAA Paper 07-0264, 2007
  • R. Rudnik, E. Germain: "Re-No. Scaling Effects on the EUROLIFT High Lift Configurations". AIAA Paper 07-0752, 2007
  • R. Rudnik: "Final Report EUROLIFT 2 Project".AST3-CT04-502896, 2007
  • J. Wild etal.: "Advanced High-Lift Design by Numerical Methods and Wind Tunnel Verification within the European Project EUROLIFT II". AIAA-2007-4300, 2007
  • J. Wildet al.: "Applying numerical optimization to realistic high lift design of transport aircraft –an overview of the aerodynamic design optimization investigation within the EUROLIFT II Project". Proceedings of the EUROGEN conference Munich, Germany, 2005

Technologies to control the flow conditions on wing trailing edges (TS4)

  • Outputs from AFLoNext
  • D. Sarkorov , A. Seifert, I. Detenis, S. Bauminger, and M. Steinbuch;“ Active Flow Control and Part Span Slat Interactions”, IACAS 2015, 25-26 February 2015
  • D. Dolgopyat, A. Seifert, “Conventional Airfoil Active Flow Control “Virtual” Maneuvering System”, IACAS 2015, 25-26 February 2015

  • D. Sarkorov,  A. Seifert, I. Detenis, S. Bauminger, M. Steinbuch, “Active Flow Control and Part Span Slat Interactions”, AIAA 2015, 5-9 January 2015


  • General references
  • A.D. Gardner, J. Nitzsche: Neumann, K. Richter, H. Rosemann, R. Voss, "Adaptive load redistribution using mini-teds", ICAS 2006-3.9.1, September 2006
  • K. Richter, H. Rosemann: " Experimental investigation of trailing-edge devices at transonic speeds", The Aeronautical Journal of the Royal Aeronautical Society, pp185-193, 2002
  • H. Hansen: "Application of Adaptive Trailing Edge Elements the AWIATOR Project", CEAS/KATnet conference on Key Aerodynamic Technologies, Bremen, 20-22 June, 2005
  • A. Schröder: "PIV and BOS measurements at an airfoil in transonic buffeting with flow control", EU AVERT Project, http://www.dlr.de/as/en/desktopdefault.aspx/tabid-183/251_read-19210
  • S.N. Michie: "A design methodology for circulation control manoeuvre effectors", PhD Thesis, University of Manchester, 2008
  • C.D. Harley, P I Wilde, W.J. Crowther: "Application of Circulation Control manoeuvre effectors for three axis control of a tailless flight vehicle". 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, AIAA-2009-146. 2009
  • C. Warsop: "An overview of the BAE Systems FLAVIIR Integrated UAV Research Programme". ICAS workshop on "UAV-Airworthiness, certification and access to the airspace", Seville, Sept 2007
  • S. Nathan: "The Engineer Awards - The 2011 Aerospace winner – FLAVIIR", http://www.theengineer.co.uk/awards-2011/the-2011-aerospace-winner-flaviir/1011119.article
  • K. Richter, H. Rosemann: "Steady aerodynamics of miniature trailing-edge devices in transonic flows". J. of Aircraft Vol. 49 No. 3, 898-910, 2012

Technologies to mitigate airframe noise during landing (TS5)

  • Outputs from AFloNext
  • M. Bauer, A. Büscher, and M. Pott-Pollenske; “ AFLoNext –A European Contribution to Airframe Noise Control”, INTERNOISE 2014, 16-19 November 2014

  • General references
  • J. Reichenberger: "Measured and Analysed Scaled Aircraft Model Noise Reduction Solutions Test Data and Effectiveness Assessment". RAIN-TR-03.2-02-R3/DC/1
  • J. Reichenberger, R. Drobietz: "Experimentelle Studie zum aeroakus-tischen Quellmechanismus Seitenkantenlärm". FREQUENZ, Berichts-Nr. 124 – 2008
  • W. Dobrzynski et al.: "Experimental Assessment of Low Noise Landing Gear Components". AIAA-2009-3276, 15th AIAA/CEAS Aeroacoustics Conference, May 2009, Miami, USA
  • W. Dobrzynski et al.: "Design and testing of low noise landing gears". International Journal of Aeroacoustis, Volume 5, No. 3, September 2006, pp. 233-262
  • W. Dobrzysnki : "Almost 40 years of airframe noise research - What did we achieve ?". Keynote lecture at 14th AIAA/CEAS Aeroacoustics Conference, 5-7 May 2008, Vancouver, Canada

Technologies to mitigate/control vibrations in the undercarriage area (TS6)

  • Outputs from AFLoNext
  • S.-H. Peng, A. Jirasek, M. Dalenbring, P. Eliasson, “Aerodynamic Excitation on MLG Door Exposed to Vortices Emanating from NLG of an Aircraft Model”, AIAA Aviation 2016, 13-17 June 2016
  • M. Tomac, A. Rizzi, “CFD Predictions of Unsteady Aero-Loads from Vortex Shedding on A-320 Landing Gear Door”, AIAA SciTech Forum 2016, 4-8 January 2016


  • General references
  • R. B. Langtry, P. R. Spalart: "DES Investigation of a Baffle Device for Reducing Landing-Gear Cavity Noise". 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 7 - 10 January 2008
  • J. E. Rossiter: "Wind Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds". Aeronautical Research Council, Reports and Memoranda 3438, London, 1964
  • S. H. Peng: "Simulation of Turbulent Flow Past a Rectangular Open Cavity Using DES and Unsteady RANS". AIAA paper 2006-2827, June 2006
  • V. Petitjean, J. Barron: "Parametric uncertainties in dynamic models for aeronautical structures ". International Conference on Noise and Vibration Engineering
  • I. J. Pritchard: "An Overview of Landing Gear Dynamics". NASA/TM-1999-209143. ARL-TR-1976