Aerodynamic Analysis of Aircraft Wing

p. 68-75

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Main Authors: Nguyen, Minh Triet, Nguyen, Ngoc Viet, Pham, Manh Thang
Format: Article
Language:English
Published: H. : ĐHQGHN 2017
Subjects:
Online Access:http://repository.vnu.edu.vn/handle/VNU_123/55921
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Institution: Vietnam National University, Hanoi
Language: English
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spelling oai:112.137.131.14:VNU_123-559212017-09-30T12:36:53Z Aerodynamic Analysis of Aircraft Wing Nguyen, Minh Triet Nguyen, Ngoc Viet Pham, Manh Thang Aerodynamic airfoil lift and drag UAVs p. 68-75 Aerodynamic problems in general are often difficult to solve by analytics analysis. Experimental or numerical simulation can be used to analyze these computational models. However, due to the large expenses required in the experimental method, the numerical method is more preferred. This paper presents the modeling and simulating processes of computational fluid dynamic (CFD) problem on a aircraft wing model, using typical section as NACA 2412 airfoil. This wing model might be chosen in the future experimental design. ANSYS Fluent is used to analyze the pressure and velocity distribution on the surface of wing. The lift and drag forces are also determined by ANSYS Structural. Additionally, the coefficients of lift and drag forces can be calculated through the data obtained when the relative velocity inlet between the airflow and airfoil changes from 0 to 50 m/s. The numerical results shown are compatible with those of the theory, thus suggesting a reliable alternative to predict the aerodynamic characteristics of the tested wing model in fabricating the Unmanned Aircraft Vehicles (UAVs). 2017-08-09T02:20:00Z 2017-08-09T02:20:00Z 2015 Article 2588-1124 http://repository.vnu.edu.vn/handle/VNU_123/55921 en Vol. 31;No. 2 (2015) application/pdf H. : ĐHQGHN
institution Vietnam National University, Hanoi
building VNU Library & Information Center
country Vietnam
collection VNU Digital Repository
language English
topic Aerodynamic
airfoil
lift and drag
UAVs
spellingShingle Aerodynamic
airfoil
lift and drag
UAVs
Nguyen, Minh Triet
Nguyen, Ngoc Viet
Pham, Manh Thang
Aerodynamic Analysis of Aircraft Wing
description p. 68-75
format Article
author Nguyen, Minh Triet
Nguyen, Ngoc Viet
Pham, Manh Thang
author_facet Nguyen, Minh Triet
Nguyen, Ngoc Viet
Pham, Manh Thang
author_sort Nguyen, Minh Triet
title Aerodynamic Analysis of Aircraft Wing
title_short Aerodynamic Analysis of Aircraft Wing
title_full Aerodynamic Analysis of Aircraft Wing
title_fullStr Aerodynamic Analysis of Aircraft Wing
title_full_unstemmed Aerodynamic Analysis of Aircraft Wing
title_sort aerodynamic analysis of aircraft wing
publisher H. : ĐHQGHN
publishDate 2017
url http://repository.vnu.edu.vn/handle/VNU_123/55921
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