Effect of wing type on wigcraft performance

Document Type : Original Article

Authors

1 persian gulf university

2 Department of Marine Engineering, Faculty of Engineering, Persian Gulf University, Boushehr, Islamic Republic of Iran

Abstract

Wigcrafts are vessels that fly by force from surface or wall effect. This phenomenon arises from the compression of the trapped air between the wing and the surface, which in the case, this surface is the sea. In this paper, the performance of Wigcrafts under the influence of wing geometry is evaluated. The wing has been fixed with three types of progressive designs, swept forward, swept back and rectangular wing with 4° mounting angle to the body. The hull and tail of the vessel are the same in all three models. The angle of sweep forward and sweep back wing is 45 degrees. Conceptual design with IGES format in AutoCAD software. Numerical calculations are simulated in the star CCM+ software assuming a non-uniform flow, k Epsilone Tourbulent, and in two phases with the aulerian multi-phazes model. The surface of the water is flat and without waves. The dimensionless parameters of the lift, drag and torque of all three models were compared. In the discussion of stability, only the pitch of all three vessels is free. From the free surface view, pressure contours, shear stress and sheil friction are presented on the model and water level in all three simulations. The results of all three are similar. The results of all three simulations are summarized and examined by the assumptions of flying bodies and the aerodynamics laws of different wing designs.

Keywords

Main Subjects


[1] اندرسون، جان دی، اصول آئرودینامیک، صدر عاملی، مسعود، مترجم، مؤسسه چاپ Ùˆ انتشارات دانشگاه امام‌حسین(ع).##[2] Wei,Yang., Cheng, Jiong Ying., Zhigang, Yang., Aerodynamic study of WIG craft near curved ground, Shanghai Automotive Wind Tunnel Center, Tongji University, Shanghai , China.##[3] Liang, Yun. Bliault, Alan. Doo, Johnny. WIG Craft and Ekranoplan Ground Effect Craft Technology, Springer New York Dordrecht Heidelberg London, May 2009.##[4] Chun,H.H., Chang,C.H., Longitudinal stability and dynamic motions of a small passenger WIG craft, Department of Naval Architecture & Ocean Engineering, Pusan National University, September 2001.##[5] Anderson, J. D., AIRCRAFT PERFORMANCE AND DESIGN, Tata McGraw-Hill Edition 2010.## [6] Hiemcke, C., Design of a wing section in ground effect, application to high speed ground transportation Iowa State University.##[7] Divitiis, N, D., PERFORMANCE AND STABILITY OF A WINGED VEHICLE IN GROUND EFFECT University of Rome “La Sapienza”, Rome, Italy.##[8] Cui, Erjie., Zhang, X., Ground Effect Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing, China School of Engineering Sciences, University of Southampton, Southampton, UK.##[9] Nilsson, E., Airfoil Optimization through Di_erential Evolution October 22/2017##[10] Wei Yang* WIG craft serves niche transportation needs Shanghai Automotive Wind Tunnel Centre, Tongji University, Shanghai 201804, China E-mail: david_ yangwei @yahoo.cn.##[11] Paul A. Czysz Department of Aerospace & Mechanical Engineering, Saint Louis University, St. Louis, MO 63103-1110, USA E-mail: paulczysz@sbcglobal.net##[12] Geok Hean AM90 Wing In Ground (WIG) Aircraft – Aerodynamics Submitted by Ng Department of Mechanical Engineering In partial fulfilment of the requirements for the Degree of Bachelor of Engineering National University of Singapore Session 2004/2005.##[13] Wei YangWIG craft serves niche transportation needs Article in World Review of Intermodal Transportation Research · August 2011.##[14]Experimental investigation of wing-in-ground effect with a NACA6409 section, Kwang Hyo Jung Æ Ho Hwan Chun Æ Hee Jung Kim, Received: 4 October 2007 / Accepted: 25, April 2008 / Published online: 12 August 2008_ JASNAOE 2008##