A study on performance of planing-wing hybrid craft

1. Matveev K. I., Dubrovsky V. A.: Aerodynamic Characteristicsof a Hybrid Trimaran Model. Ocean Engineering, 34(3-4),2007.10.1016/j.oceaneng.2006.04.001Search in Google Scholar

2. Shipps, P. R.: Hybrid ram-wing/planning craft - today’sraceboats, tomorrow’s outlook. AIAA/SNAME Advanced Marine Vehicles Conference, 197610.2514/6.1976-877Search in Google Scholar

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, 1978Search in Google Scholar

4. Privalov, E. I., Kirillovikh, V. N.: Transport amphibiousplatforms: a new type of high-speed craft. Proceedings of Ekranoplans & Very Fast Craft Workshop, 1996Search in Google Scholar

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, 1997Search in Google Scholar

6. www.freepatentonline.comSearch in Google Scholar

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, UKSearch in Google Scholar

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, 2007Search in Google Scholar

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, 200810.3940/rina.hsmv.2008.01Search in Google Scholar

10. www.seaphantom.comSearch in Google Scholar

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.Search in Google Scholar

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, 2008Search in Google Scholar

13. Matjasic K. at al.: WIG (Wing In Ground effect) craft in militaryand paramilitary applications. NATO Conference, TO-AVT Symposium, April 7 -11, 2003Search in Google Scholar

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. 2578~2589,10.1007/s12206-008-0805-ySearch in Google Scholar

15. Husa B.: WIG configuration development from componentmatrix. Orion technology, Aerospace design and engineering, Internal report, 2000Search in Google Scholar

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, 2010Search in Google Scholar