Paper Titles in Periodical
International Letters of Chemistry, Physics and Astronomy
ILCPA Volume 55
Subscribe

Subscribe to our Newsletter and get informed about new publication regulary and special discounts for subscribers!

ILCPA > ILCPA Volume 55 > Manufacturing FX 63-137 Aerofoil by Using CNC...
Manufacturing FX 63-137 Aerofoil by Using CNC Machine and Determine Aerodynamic Characteristic for this Aerofoil
< Back to Volume

Manufacturing FX 63-137 Aerofoil by Using CNC Machine and Determine Aerodynamic Characteristic for this Aerofoil

Full Text PDF

Abstract:

The aim of this paper is to manufacturing and testing FX 63-137 aerofoil at different speed by using experimental wind tunnel , and select best angel of attack. This paper uses an approach in which the process is divided into many steps. Firstly, manufacturing aerofoil by using CNC Machine. Secondly, testing the aerofoil by using Wind Tunnel, Finally display and compare results with another reference results with to evaluate the solutions are studied and the up-scaling rule which is a way to get some general insight for this aerofoil.

Info:

Periodical:
International Letters of Chemistry, Physics and Astronomy (Volume 55)
Pages:
119-127
DOI:
https://doi.org/10.18052/www.scipress.com/ILCPA.55.119
Citation:
M. M. M. Saad and N. binti Ismail, "Manufacturing FX 63-137 Aerofoil by Using CNC Machine and Determine Aerodynamic Characteristic for this Aerofoil", International Letters of Chemistry, Physics and Astronomy, Vol. 55, pp. 119-127, 2015
Online since:
July 2015
Authors:
Magedi Moh. M. Saad, Norzelawati binti Ismail
Keywords:
Angle of Attack, Drag, Lift, Wind Tunnel
Export:
RIS, BibTeX, Text
Distribution:
Open Access

Creative Commons License
This work is licensed under a
Creative Commons Attribution 4.0 International License

References:

Xin, H., Chunhua, Z., Guoqing, Z., Ping, W. & XiChun, Z. (2012). High altitude and long endurance unmanned aerial vehicle bionic airfoil research, at. Paper read at Electronic System-Integration Technology (ESTC), 2 12 4th: 1568-1571. 7-20 Sept.

Jianjun, Q., Yi, M. & Mingwei, X. (2011 ). Investigation on Performance Influence of Maximum Thickness Position on Vertical Axis Wind Turbine Airfoil, at. Paper read at Power and Energy Engineering Conference APPEE, Asia Paci c: 1-4. 2 -28.

Caughey, David A. (2011). Introduction to Aircraft, Stability and Con ol Course Notes for M&A 5 70..

Radespiel, Rolf E., Jan Windte, and Ulrich Scholz. (2007). Numerical and experimental flow analysis of moving., airfoils withlaminar flow and . low number AIAA journ l45. 6: 1346-1356qq.

A. Gustafson. (2011). 'Design, Simulation, and Wind Tunnel Verification of a Morphing Airfoil',. Thesis submitted to the Faculty of the Virginia Polytechnic Institute and State University in partial.

Jianjun, Q., Yi, M. & Mingwei, X. (2011 ). Investigation on Performance Influence of Maximum Thickness Position on Vertical Axis Wind Turbine Airfoil, at. Paper read at Power and Energy Engineering Conference (APPEEC).

Yang, Cher-Chiang. (2008). Low Speed Virtual Wind Tunnel Simulation For Educational Studies In Introducing Computational Fluid Dynamics And Flow Visualization.

T. J. Blackwell (2011). SUBSONIC WIND-TUNNEL WALL CORRECTIONS ON A WING. Diss. San Jose.

Allan, Brian G., Greg S. Jones, and John C. Lin. (2011). Simulation of a 2D Wind Tunnel Experiment., 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper.

Show More Hide
Cited By:
This article has no citations.