Nowadays, together with the huge development in information technology, the use of numerical method is no longer an obstacle. It provides a lot of advantages such as providing high precise solutions, reducing time and cost for designing and manufacturing flying vehicle models and dealing with extremely complex problems by using physical models compared to the usual analytical methods. The operation of airplanes represents a critical aerodynamic practical problem due to the wing. Interference this article presents a method to identify the aerodynamics coefficients of flying vehicles for isolate wing using software ANSYS. CFX and compares obtained results to the with those received by analytical method.
| Published in | Automation, Control and Intelligent Systems (Volume 3, Issue 6) |
| DOI | 10.11648/j.acis.20150306.14 |
| Page(s) | 118-123 |
| Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
| Copyright |
Copyright © The Author(s), 2015. Published by Science Publishing Group |
Aerodynamic Characteristics, Wing, Airfoil Section, Angle of Attack
| [1] | Ansys. CFX Release 12.0: ANSYS CFX-Solver Theory Guide. |
| [2] | Ansys. Gambit Helps. |
| [3] | Zakharchenko VF, et al., Determination of total aerodynamic characteristics of various configurations of aircraft. M: Publishing house of the MSTU. Bauman, 1993. |
| [4] | AA Lebedev, Chernobrovkin LS Flight Dynamics: unmanned aerial vehicles. M: Mechanical Engineering, 1973. |
| [5] | Process and research on the method of guidance a maneuvering target with scholastic prediction about its motion and with nonlinearities in the control circle” (A report on the scientific researching work)/MSTU named after Bauman. The supervisor: Pupkov K. A. The executors: Nguyen Quang Vinh, Bobkov A. V., Ustiuzanin A. D. / Moscow, 2006, 75 pages. |
APA Style
Nguyen Quang Vinh. (2015). Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Automation, Control and Intelligent Systems, 3(6), 118-123. https://doi.org/10.11648/j.acis.20150306.14
ACS Style
Nguyen Quang Vinh. Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Autom. Control Intell. Syst. 2015, 3(6), 118-123. doi: 10.11648/j.acis.20150306.14
AMA Style
Nguyen Quang Vinh. Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Autom Control Intell Syst. 2015;3(6):118-123. doi: 10.11648/j.acis.20150306.14
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Download@article{10.11648/j.acis.20150306.14,
author = {Nguyen Quang Vinh},
title = {Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS},
journal = {Automation, Control and Intelligent Systems},
volume = {3},
number = {6},
pages = {118-123},
doi = {10.11648/j.acis.20150306.14},
url = {https://doi.org/10.11648/j.acis.20150306.14},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.acis.20150306.14},
abstract = {Nowadays, together with the huge development in information technology, the use of numerical method is no longer an obstacle. It provides a lot of advantages such as providing high precise solutions, reducing time and cost for designing and manufacturing flying vehicle models and dealing with extremely complex problems by using physical models compared to the usual analytical methods. The operation of airplanes represents a critical aerodynamic practical problem due to the wing. Interference this article presents a method to identify the aerodynamics coefficients of flying vehicles for isolate wing using software ANSYS. CFX and compares obtained results to the with those received by analytical method.},
year = {2015}
}
TY - JOUR T1 - Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS AU - Nguyen Quang Vinh Y1 - 2015/12/22 PY - 2015 N1 - https://doi.org/10.11648/j.acis.20150306.14 DO - 10.11648/j.acis.20150306.14 T2 - Automation, Control and Intelligent Systems JF - Automation, Control and Intelligent Systems JO - Automation, Control and Intelligent Systems SP - 118 EP - 123 PB - Science Publishing Group SN - 2328-5591 UR - https://doi.org/10.11648/j.acis.20150306.14 AB - Nowadays, together with the huge development in information technology, the use of numerical method is no longer an obstacle. It provides a lot of advantages such as providing high precise solutions, reducing time and cost for designing and manufacturing flying vehicle models and dealing with extremely complex problems by using physical models compared to the usual analytical methods. The operation of airplanes represents a critical aerodynamic practical problem due to the wing. Interference this article presents a method to identify the aerodynamics coefficients of flying vehicles for isolate wing using software ANSYS. CFX and compares obtained results to the with those received by analytical method. VL - 3 IS - 6 ER -
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