Investigation of Wings in Ground Effect using Computational Fluid Dynamics

Gulraiz Ahmed

Published by GRIN Verlag Gmbh Sep 2013, 2013
ISBN 10: 3656231184 / ISBN 13: 9783656231189
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Neuware - Master's Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormousvoid between speed of an aircraft and the payload capacity of a ship. WIG vehicleswould be able to move cargo and passengers faster than a ship and more economicalthan an aircraft. Ground effect is a phenomenon that occurs on all wings flying closeto the ground or a surface.The aim of this project is to investigate the behavior of wings (NACA/DHMTU series)in ground effect (on a fixed/variable terrain) using Fluent CFD package. The NACA0012 and DHMTU series used in this project are designed specifically to fly in closeproximity to the ground.The performance of the NACA/ DHMTU airfoils is examined for the lift and the dragcoefficients at different altitudes with varying angle of attack. The results arecompared to experimental data that is available to assess the accuracy of the CFDsimulation. 92 pp. Englisch. Bookseller Inventory #

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Synopsis: Master's Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormous void between speed of an aircraft and the payload capacity of a ship. WIG vehicles would be able to move cargo and passengers faster than a ship and more economical than an aircraft. Ground effect is a phenomenon that occurs on all wings flying close to the ground or a surface. The aim of this project is to investigate the behavior of wings (NACA/DHMTU series) in ground effect (on a fixed/variable terrain) using Fluent CFD package. The NACA 0012 and DHMTU series used in this project are designed specifically to fly in close proximity to the ground. The performance of the NACA/ DHMTU airfoils is examined for the lift and the drag coefficients at different altitudes with varying angle of attack. The results are compared to experimental data that is available to assess the accuracy of the CFD simulation.

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Title: Investigation of Wings in Ground Effect ...
Publisher: GRIN Verlag Gmbh Sep 2013
Publication Date: 2013
Binding: Taschenbuch
Book Condition: Neu

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Book Description GRIN Verlag. Paperback. Book Condition: New. Paperback. 92 pages. Dimensions: 8.2in. x 5.8in. x 0.3in.Masters Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormous void between speed of an aircraft and the payload capacity of a ship. WIG vehicles would be able to move cargo and passengers faster than a ship and more economical than an aircraft. Ground effect is a phenomenon that occurs on all wings flying close to the ground or a surface. The aim of this project is to investigate the behavior of wings (NACADHMTU series) in ground effect (on a fixedvariable terrain) using Fluent CFD package. The NACA 0012 and DHMTU series used in this project are designed specifically to fly in close proximity to the ground. The performance of the NACA DHMTU airfoils is examined for the lift and the drag coefficients at different altitudes with varying angle of attack. The results are compared to experimental data that is available to assess the accuracy of the CFD simulation. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN. Paperback. Bookseller Inventory # 9783656231189

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Book Description GRIN Publishing, United States, 2012. Paperback. Book Condition: New. 1. Auflage.. 210 x 148 mm. Language: English . Brand New Book ***** Print on Demand *****.Master s Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormous void between speed of an aircraft and the payload capacity of a ship. WIG vehicles would be able to move cargo and passengers faster than a ship and more economical than an aircraft. Ground effect is a phenomenon that occurs on all wings flying close to the ground or a surface. The aim of this project is to investigate the behavior of wings (NACA/DHMTU series) in ground effect (on a fixed/variable terrain) using Fluent CFD package. The NACA 0012 and DHMTU series used in this project are designed specifically to fly in close proximity to the ground. The performance of the NACA/ DHMTU airfoils is examined for the lift and the drag coefficients at different altitudes with varying angle of attack. The results are compared to experimental data that is available to assess the accuracy of the CFD simulation. Bookseller Inventory # APC9783656231189

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