References
- 1. Matveev K. I., Dubrovsky V. A.: Aerodynamic Characteristicsof a Hybrid Trimaran Model. Ocean Engineering, 34(3-4),2007.
- 2. Shipps, P. R.: Hybrid ram-wing/planning craft - today’sraceboats, tomorrow’s outlook. AIAA/SNAME Advanced Marine Vehicles Conference, 1976
- 3. Ward, T. M., Goelzer, H. F., Cook, P. M.: Design andperformance of the ram wing planning craft - KUDU II. AIAA/ SNAME Advanced Marine Vehicles Conference, 1978
- 4. Privalov, E. I., Kirillovikh, V. N.: Transport amphibiousplatforms: a new type of high-speed craft. Proceedings of Ekranoplans & Very Fast Craft Workshop, 1996
- 5. Doctors, L. J.: Analysis of the efficiency of an ekranocat:a very high speed catamaran with aerodynamic alleviation. International Conference on Wing In Ground Effect Craft (WIGs ‘97), RINA, 1997
- 6. www.freepatentonline.com
- 7. Collu M., Patel M. H., Trarieux F.: High speed marine vehicleswith aerodynamic surfaces: development of a dynamic model fora novel configuration. Cranfield Multi Strand Conference, 6-7 May 2008. Cranfield, Bedfordshire, UK
- 8. Collu M., Patel M. H., Trarieux F.: A Unified MathematicalModel for High Speed Hybrid (Air and Waterborne)Vehicles., 2nd International Conference on Marine Research and Transportation, 2007
- 9. Collu M., Patel M. H., Trarieux F.:A Mathematical Model toanalyze the Static Stability of Hybrid (Aero hydrodynamicallysupported) vehicles. 8th Symposium on High Speed Marine Vehicles 2008 (HSMV08), Naples, Italy, 2008
- 10. www.seaphantom.com
- 11. Korneev, N.V., Taranov, A.E., Treshkov, V.K.: Efficient softwarefor numerical calculation of ekranoplans (WIG craft) andhydrofoils. Proc. Workshop WISE up to Ekranoplan GEMS,The University of New South Wales, Sydney, Australia, pp. 263-266, 1998.
- 12. Bakhshandehrostamai A. Ghasemi H.: Design and Analysisof 2D Wing In Ground Effect Based on Maximum Lift-DragRatio.,MSc thesis, Amirkabir University of Technology, Tehran, Iran, 2008
- 13. Matjasic K. at al.: WIG (Wing In Ground effect) craft in militaryand paramilitary applications. NATO Conference, TO-AVT Symposium, April 7 -11, 2003
- 14. Park K. and Lee J.: Influence of endplate on aerodynamiccharacteristics of low-aspect-ratio wing in ground effect. Journal of Mechanical Science and Technology, Vol.22, 2008, pp. 2578~2589,
- 15. Husa B.: WIG configuration development from componentmatrix. Orion technology, Aerospace design and engineering, Internal report, 2000
- 16. Yun L. Bliault A., Doo J.: WIG craft and Ekranoplan; Groundeffect craft technology. ISBN 978-1-4419-0041-8 e-ISBN 978- 1-4419-0042-5, Springer, 2010