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Barlow, Chris; Lewis, Darren; Prior, Stephen D.; Odedra, Sid; Erbil, Mehmet Ali; Karamanoglu, Mehmet; Collins, R. (2009)
Publisher: International Conference on Manufacturing and Engineering Systems.
Languages: English
Types: Article
Subjects:
In recent years the demand for Unmanned Aerial Vehicles(UAV's) has increased rapidly across many different industries and they are used for various applications. Such systems have the ability to enter dangerous or inaccessible environments and allow vital information to be collected without human risk.\ud In order to carry out a task, a UAV has to face many\ud different challenges. This has led to the development of novel platforms that move away from traditional aircraft design in order to make them more capable. A good example of this type of craft is one which uses the Coanda Effect to assist propulsion. This effect was discovered in 1930 by Henri-Marie Coanda who found that if a thin film of air is directed over a curved body, then the air follows the curve. When used to propel a UAV, the Coanda Effect also\ud entrains air from above and lowers the air pressure in this region, which in turn generates more lift.\ud Many organizations have attempted to use this\ud phenomenon to aid the lift of various unusual air vehicles.
  • The results below are discovered through our pilot algorithms. Let us know how we are doing!

    • [1] Van Blythenburg, P. (2009). UAS Yearbook - UAS: The Global Perspective (2009-2010). 7th Edition. Blythenburgh & Co. Paris, France.
    • [2] Aesir Ltd. (2009). Defence. Retrieved 19 October 2009 from AESIR Unmanned Autonomous Systems: http://www.aesiruas.com/markets_defence.htm.
    • [3] Coanda, H. (1938). Propelling Device. US Patent Office, US Patent # 2,108.652.
    • [4] Day, T. (2008). The Coanda Effect and Lift. Retrieved from New Fluid Technology: http://www.newfluidtechnology.com.au/THE_COANDA_EF FECT_AND_LIFT.pdf.
    • [5] Coanda, H. (1936). Device for Deflecting a Stream of Elastic Fluid Projected into an Elastic Fluid. US Patent Office, US Patent # 2,052,869.
    • [6] Anderson, D.1 & S. Eberhardt2 (2009). A Physical Description of Flight; Revisited. Retrieved from Aeronautics Learning Laboratory for Science Technology and Research: www.allstar.fiu.edu/aero/Flightrevisited.pdf.
    • [7] Aesir Ltd. (2009). Explanation of the Technology. Retrieved 19 October 2009 from AESIR Unmanned Autonomous Systems: http://www.aesir-uas.com/technology.htm.
    • [8] Naudin, J.L. (2006). The GFS Retrieved 19 October 2009 from JLN http://jlnlabs.online.fr/gfsuav/gfsuavn01a.htm. UAV Project. Labs Online:
    • [9] Bellot, J. Oswald, R. & L. Segessemann (2009). Simulation, Construction and Optimisation of an Unmanned Aerial Vehicle Based on the Coanda Effect. Maturaarbeit (A-Level work) 2009, Literargymnasium Rämibühl, Zürich, Switzerland.
    • [10] Collins, R. (2003). Aerial Flying Device. UK Patent Office, Patent # GB 2,387,158.
    • [11] Collins, R. (2008). Unmanned Coanda Disk Aircraft System Platform. Retrieved 19 October 2009 from Create the Future Design Contest: http://www.createthefuturecontest.com/pages/view/entriesdet ail.html?entryID=1961#at.
    • [12] Dyson Ltd. (2009). Air Multiplier™ Technology. Retrieved 19 October 2009 from Dyson: http://www.dyson.co.uk/technology/airmultiplier.asp#HowIt Works.
    • [13] Lyon, C.A. Broeren, A.P. Giguere, P. Gopalarathnam, A. & M.S. Selig (1996). Summary of Low-Speed Airfoil Data - Volume 2. SoarTech Publications, Virginia Beach, USA.
    • [14] Schroijen, M.J.T. & M.J.L. van Tooren (2009). MAV Propulsion System using the Coanda Effect. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, Colorado, Aug. 2-5, 2009.
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