Skip to main content Accessibility help
×
Hostname: page-component-848d4c4894-ndmmz Total loading time: 0 Render date: 2024-05-17T04:17:55.911Z Has data issue: false hasContentIssue false

11 - Aerodynamic Air Cushion Craft

Published online by Cambridge University Press:  05 October 2015

Get access

Summary

“Speed, bonnie boat, like a bird on the wing”

Skye Boat Song

Harold Edwin Boulton (1859–1935)

Before proceeding with this Chapter, the reader might pause for a moment and glance again at the photograph in Figure 2.1 in Chapter 2 and imagine a wing-in-ground-effect (WIG) craft (or “ship”) flying close to the water to obtain the lift advantage from “ground or surface effect” in those same sea conditions. One might also wonder why all the photographs that have appeared in the literature from the small personal aircraft using the WIG principle to the largest sizes in the Russian, Chinese and German work on WIG, and with the US PAR WIG and other variants of wing-in-ground-effect, are all taken in calm waters or in relatively calm seas. This is a problem that needs to be addressed and will be referred to in this chapter on this promising concept to achieve high speed over the seas of the world.

Aerodynamic Underpinnings

The basic aerodynamic principles that apply to aerodynamic air cushion craft can be traced to before the Wright brothers first flew at Kitty Hawk on 17 December 1903. In the late 1800s several scientists and renowned engineers were developing the theory of flight and building practical man-powered gliders. Sir George Cayley (1773–1857) in Scarborough, Yorkshire, England is frequently referred to as “the father of aeronautics” because of his extensive work in determining the four basic forces for flight: lift, drag, thrust and weight and building the first glider to carry a man aloft. The first flight was in 1849 with a young boy as pilot. A much larger glider that flew across Brompton Dale (near Scarborough, Yorkshire) was in 1853 with a grown man as pilot. Historical records are not clear as to who the pilot was but possibly an employee or probably Sir Cayley's grandson. A history of Sir George Cayley and his work may be found in Richard Dee's excellent 2007 book.1 Sir George Cayley was a prolific inventor and well versed in basic research methods. An interesting and prescient set of short articles written by him appears in the 1809 and 1810 Journal of Natural Philosophy2 where he outlines the governing principles for flight.

Type
Chapter
Information
High-Speed Marine Craft
One Hundred Knots at Sea
, pp. 501 - 586
Publisher: Cambridge University Press
Print publication year: 2015

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Dee, Richard, “The Man who Discovered Flight: George Cayley and the First Airplane”, published by McClelland & Stewart, Toronto, (2007)
2. Cayley, George, “On Aerial Navigation”, Nicholson's Journal of Natural Philosophy, Published in three issues (Part 1: November 1809; Part 2: February 1810; and Part 3: March 1810).
3. Lilienthal, Otto; “Der Vogelflug als Grundlage der Fliegekunst” pub by Gaertners, R. Verlagsbuchhandlung, 1889. Later translated by Isenthal, I.W. as Birdflight as the Basis of Aviation, and published by Longmans, Green; London 1911
4. Lanchester, Frederick W.; “Aerodynamics”, published by Constable & Co., London 1907Google Scholar
5. Helmholtz, Hermann L., “On the Integrals of the Hydrodynamic Equations Corresponding to Vortex Motions”, published in Crelles Journal fϋr die reine und angewandte Mathematik 60, pp23–55, 1858
6. Giacomelli, R. and Pistolesi, E., “Historical Sketch” in “Aerodynamic Theory”, Vol 1 ed. Durand, W.F., pub by Springer, Berling 1934CrossRefGoogle Scholar
7. Prandtl, Ludwig; “Tragflächentheorie” (Wing Theory), I Mitteilung (Note I) Nachrichten der K. Gesellschaft der Wissenschaften zu Göttingen, Math-phys. Klasse, 1918. Note II published in 1919.
8. Glauert, Hermann, “The Elements of Aerofoil and Airscrew Theory”, Cambridge University Press, 1926Google Scholar
9. Glauert, Hermann, “The Calculation of the Characteristics of Tapered Wings”, British R&M 767, 1921–1922
10. Jones, Robert T., “Theoretical Correction for the Lift of Elliptical Wings”, Jnl Aeronautical Sciences, 9, No 1, 8, November 1941
11. Jones, Robert T., “Corrections of the Lifting Line Theory for the Effect of Chord”, NACA Tech Note 817, July 1941
12. Glauert, Hermann, “The Elements of Aerofoil and Airscrew Theory”, Cambridge University Press, 1926Google Scholar
13. Betz, Albert, “Lift and Drag of a Wing near a Horizontal Surface (the ground)”, published in Zeitschrift fϋr Flugtechnik und Motorluftachiffahrt”, 1912
14. Wieselsberger, Carl; “Über den Flugwiderstand in der Nähe des Boden” (Wing Resistance Near the Ground) originally published in Zeitschrift fϋr Flugtechnik und Motorluftschiffahrt, Vol No.10, p145, 1921. Translated and published as NACA Technical Memorandum No. 77, April 1922
15. Fink, Marvin P. and Lastinger, James L., “Aerodynamic Characteristics of Low Aspect Ratio Wings in Close Proximity to the Ground”, NASA Technical Note D-926, July 1961.
16. Carter, Arthur W., “Effect of Ground Proximity on the Aerodynamic Characteristics of Aspect Ratio 1 Airfoils With and Without End Plates”, NASA Technical Note D-970, October 1961
17. NACA Report: “Aerodynamic Characteristics of Airfoils–IV”, NACA Report 244, published 1926
18. Cockerell, C.S., “Ripplecraft”, Report 1/55 (25 October 1955). See also Air Cushion Vehicle Supplement to Flight International Magazine, 28 February 1963.
19. Mantle, Peter J., “Air Cushion Craft Development”, US Navy Report No. DTNSRDC-80–012, January 1980
20. Stanton-Jones, Richard, “The Development of the Saunders-Roe Hovercraft SR.N1”, Symposium on Ground Effect Phenomena at Princeton, Paper 13 (21–23 October 1959)
21. Stanton-Jones, Richard, “Some Design Problems of Hovercraft”, Institute of Aerospace Sciences Paper 61–45 (1961). Also Saunders-Roe Publication S.P.404, January 1961
22. Elsley, Gordon H. and Devereux, Anthony J., “Hovercraft Design and Construction”, published by Cornell Maritime Press, Inc., in 1968
23. Payne, Peter R., “Curved Jet Flows”, United States Army Material Laboratory Technical Report 65–20, May 1965
24. Elsley, Gordon H., “Two-Dimensional Hovercraft Lift”, Saunders-Roe Ltd, Report A/A/53, November 1958
25. Stanton-Jones, Richard, “The Development of the Saunders-Roe Hovercraft SR.N1”, Symposium on Ground Effect Phenomena at Princeton, Paper 13, 21–23 October 1959
26. Carmichael, B.H. and Southcote, M.P., “Air Cushion Feasibility Investigation, Performance and Stability Experiments, Configuration and System Evaluation Studies”, Ford Aeronutronic Co., Publication U-1066, November 1960
27. Mantle, Peter J., “Thrust and Drag Estimate for the Channel Flow GEM”, Vehicle Research Corporation report, WP 36, September 1962
28. Braunss, G. and Lincke, W., “Die Auftriebsverteilung einer Ebenen Platte in Bodennahe” (The Lift Distribution on a Flat Plate in Ground Effect) published in Journal Zeitschrift fϋr Flugwissenschaften, No. 10, 1962
29. Ashill, Peter R., “On the Minimum Induced Drag of Ground-Effect Wings”, published in The Aeronautical Quarterly, Royal Aeronautical Society, Volume XXI, Part 3, pp211–232, August 1970
30. “Wingship Investigation”, Final Report, published by Advanced Research Projects Agency (ARPA), now Defense Advanced Research Projects Agency (DARPA), Arlington, Virginia, September 1994
31. Widnall, Sheila E., and Barrows, Timothy M., “ An Analytic Solution for Two and Three-Dimensional Wings in Ground Effect”, Jnl. Fluid Mechanics, Vol 41, part 4, pp769–792, May 1970
32. Kida, T and Miyai, Y., “Minimum Induced Drag of Non-Planar Ground Effect Wings with Small Tip Clearance”, Journal of Aeronautical Quarterly, Vol XXV, pp19–36, published by Royal Aeronautical Society, February 1974
33. Ando, Shigenori and Yashiro, Haruki, “Minimum Induced Drag of Ground Effect Wings”, Journal of Hydronautics, Vol 10, No. 3, pp106–112, published by AIAA, July 1976
34. Swanborough, Gordon and Bowers, Peter, “United States Navy Aircraft Since 1911”, pub by Naval Institute Press, Annapolis, 1990
35. Crewe, Peter R., “A Review of the Seaplane Hydrodynamic Design Problems of Greatest Present Importance and Possible Solutions. Part I, Introduction and Water Performance of Streamlined Bodies”, Saunders-Roe Ltd Report H/O/112/1, May 1950
36. Gerry, Dave G., and Crewe, Peter R, “Seaplane Design Problems”, Final Report to ANVCE Project, Saunders-Roe Ltd Report SP 3920, June 1977
37. Kehoe, James W.: “Appendix: Wing-in-Ground-Effect Vehicles” to Chapter VI: The Surface Effect Ship by Butler, Edward A., Modern Ships and Craft, Naval Engineers Journal, Special Edition, February 1985
38. Chief of Naval Operations, OP-96, “Advanced Naval Vehicles Concepts Evaluation (ANVCE) Project, Vol I, II & III”, Report No CNO LTR 96/C194136, December 1979
39. “Wingship Investigation”, Final Report, published by Advanced Research Projects Agency (ARPA), now Defense Advanced Research Projects Agency (DARPA), Arlington, Virginia, September 1994
40. “Advanced Naval Vehicles Concepts Evaluation (ANVCE) Project”, Prepared by Chief of Naval Operations (OP-96), Report No. CNO LTR 96/C194136, Vols 1,2,3,4; December 1979
41. Flight International Magazine (Air Cushion Supplement) issued November 1966
42. Multi-Mode Variable Geometry Surface Effect Ship, US Patent Number 3,481,297 by Mantle, P.J. filed 13 Nov 1967, issued 2 December 1969
43. Mantle, Peter J., “Some Design Aspects of Air Cushion Craft”, paper presented at the International Congress of Subsonic Aeronautics, New York, NY, 3–6 April 1967. Published in the Annals of the New York Academy of Sciences, Vol 154, Article 2, pages 924–952, 22 November 1968Google Scholar
44. Wing in Ground Effect Vehicle, US Patent Number 4,151,893 by Mantle, Peter J., filed 8 September 1977, issued on 1 May 1979
45. http://en.wikipedia.org/wiki/Rolls-Royce_Pegasus
46. Mineck, Raymond E. and Carter, Arthur W., “Effect of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Aspect Ratio-1 Wing With and Without Wing-Tip Blowing”, NASA Technical Memorandum NASA TM X-3048, July 1974

Save book to Kindle

To save this book to your Kindle, first ensure coreplatform@cambridge.org is added to your Approved Personal Document E-mail List under your Personal Document Settings on the Manage Your Content and Devices page of your Amazon account. Then enter the ‘name’ part of your Kindle email address below. Find out more about saving to your Kindle.

Note you can select to save to either the @free.kindle.com or @kindle.com variations. ‘@free.kindle.com’ emails are free but can only be saved to your device when it is connected to wi-fi. ‘@kindle.com’ emails can be delivered even when you are not connected to wi-fi, but note that service fees apply.

Find out more about the Kindle Personal Document Service.

Available formats
×

Save book to Dropbox

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Dropbox.

Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

Available formats
×