Aircraft Design Analysis, CFD and manufacturing

Publications

Share / Export Citation / Email / Print / Text size:

International Journal of Advanced Network, Monitoring and Controls

Xi'an Technological University

Subject: Computer Science , Software Engineering

GET ALERTS

eISSN: 2470-8038

DESCRIPTION

6
Reader(s)
23
Visit(s)
0
Comment(s)
0
Share(s)

SEARCH WITHIN CONTENT

FIND ARTICLE

Volume / Issue / page

Related articles

VOLUME 1 , ISSUE 2 (December 2016) > List of articles

Aircraft Design Analysis, CFD and manufacturing

Haifa El-Sadi

Keywords : computational fluid dynamics (CFD), design, aircraft, aerodynamic, wind tunnel

Citation Information : International Journal of Advanced Network, Monitoring and Controls. Volume 1, Issue 2, Pages 59-67, DOI: https://doi.org/10.21307/ijanmc-2016-017

License : (CC BY-NC-ND 4.0)

Published Online: 02-April-2018

ARTICLE

ABSTRACT

Aircraft design, manufacturing and CFD analysis as part of aerodynamic course, the students achieve sizing from a conceptual sketch, select the airfoil geometry and the tail geometry, calculate thrust to weight ratio and wing loading, use initial sizing and calculate the aerodynamic forces. The students design their aircraft based on the geometrical dimensions resulted from the calculations and use the model to build a prototype, test it in wind tunnel and achieve CFD analysis to be compared with the experimental results. The theory of aerodynamic is taught and applied as a project based. In this paper, the design process, aircraft manufacturing and CFD analysis are presented to show the effect of project based on student’s learning of aerodynamic course. This project based learning has improved and accelerated students understanding of aerodynamic concepts and involved students in a constructive exploration.

The analysis of the aircraft resulted in a study that revolved around the lift and drag generation of this particular aircraft. As to determine the lift and drag forces generated by this plane, a model was created in Solidworks a 3-D model-rendering program. After this model was created it was 3-D printed in a reduced scale, and subjected to wind tunnel testing. The results from the wind tunnel lab experiment were recorded. For accuracy, the same 3-D model was then simulated using CFD simulation software within Solidworks and compared with the results from the wind tunnel test. The values derived from both the simulation and the wind tunnel tests were then compared with the theoretical calculations for further proof of accuracy.

Content not available PDF Share

FIGURES & TABLES

REFERENCES

Anderson, Jr., J.D., 2012, Introduction to Flight, McGraw-Hill, seventh edition

 

J.J. Bertin, Aerodynamics for Engineers, 5th ed., Prentice Hall, 2008.

 

Kuethe, A.M. and Chow, C.-Y., Foundations of Aerodynamics, 5th ed., Wiley, 1997.

 

Houghton, E.L. and Carruthers N.B., Aerodynamics for Engineering Students, 3rd ed., Arnold, 1982 .

 

Daniel P. Raymer, “Aircraft Design: A Conceptual Approach”, published by American Institute of Aeronautics and Astronautics, Inc.

 

Gennaro Zuppardi, Luigi G. Napolitano, “Teaching aerodynamics using a microcomputer”, Computers & Education, Volume 11, Issue 2, 1987, Pages 73–84 .

 

Mark Drela, “Assorted views on teaching of aerodynamics”, 16th AIAA Applied Aerodynamics Conference, AIAA-98-2792 .

 

EXTRA FILES

COMMENTS