An Investigation on Manufacture Method of High-Speed Wind-Tunnel Test Models Based on Stereo-Lithography Technique

Article Preview

Abstract:

The paper presents a novel manufacture method of high-speed wind-tunnel test models with internal metal frame and surface photopolymer resin based on Stereo-Lithography (SL) technique. Internal metal frame structure was designed to be of regular configurations that can be conveniently fabricated by conventionally mechanical manufacturing methods. Outer resin components were designed to meet configuration fidelity and surface quality, which were fabricated by SL facilities. Combination of aerodynamics and structure was utilized to accomplish structural design, strength and stiffness calibration and vibration analysis. It is validated that the manufacture method is suitable to construct the high-speed wind-tunnel models by some typical wind-tunnel models, especially for test models with complex structure.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 753-755)

Pages:

2722-2726

Citation:

Online since:

August 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Charles Tyler, WPAFB, OH, William Braisted and James Higgins. (2005), Evaluation of Rapid Prototyping Technologies for Use in Wind Tunnel Model Fabrication, AIAA Paper 2005-1301.

DOI: 10.2514/6.2005-1301

Google Scholar

[2] A. Springer and K. Cooper. (1997), Comparing the aerodynamic characteristics of wind-tunnel models produced by rapid prototyping and conventional methods, AIAA Paper 97-2222.

DOI: 10.2514/6.1997-2222

Google Scholar

[3] Hildebrand R. J, Eidson R.C. and Tyler C. (2003), Development of a low cost, rapid prototype, lambda wing-airframe wind-tunnel model, 21st Applied Aerodynamics Conference, Orlando, FL, AIAA Paper 2003-3818, pp: 23-26.

DOI: 10.2514/6.2003-3818

Google Scholar

[4] Heyes A.L. and Smith D.A.R. (2004), Rapid techniques for wind-tunnel model manufacture, Journal of Aircraft, Vol. 41 No. 2, pp: 413-415.

DOI: 10.2514/1.4730

Google Scholar

[5] Chua C. K, Leong K. F and Lim C.S. (2003), Rapid prototyping principles and applications, World Scientific, Hackensack, NJ.

Google Scholar

[6] Quincieu J, Robinson C, Stucker B and Mosher T. (2005), Case study: selective laser sintering of the USUS at II small satellite structure, Assembly Automation, Vol. 25 No. 4, pp: 267-272.

DOI: 10.1108/01445150510626389

Google Scholar

[7] Aghanajafi S, Adelnia R and Daneshmand S. (2006), Production of wind-tunnel testing models with use of rapid prototyping methods, WSEAS Transactions on Circuits and Systems, Vol. 5, No. 4, pp: 555-561.

Google Scholar

[8] Charles Tyler, William Braisted and James Higgins. (2005), Evaluation of rapid prototyping technologies for use in wind-tunnel model fabrication, AIAA Paper 2005-1301.

DOI: 10.2514/6.2005-1301

Google Scholar

[9] Zhihua Zhou and Dichen Li et al. (2008), Design and fabrication of a hybrid surface-pressure airfoil model based on rapid prototyping, Rapid Prototyping Journal, Vol. 14, No. 1, pp: 57-66.

DOI: 10.1108/13552540810841571

Google Scholar

[10] Hague, R., Mansour, S. and Saleh, N. (2004), Material and design considerations for rapid manufacturing, International Journal of Production Research, Vol. 42, No. 22, pp: 4691-4708.

DOI: 10.1080/00207840410001733940

Google Scholar

[11] Tyler, C. (2005), Evaluation of rapid prototyping technologies for use in wind tunnel model fabrication, paper presented at 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 2005-1301, 10-13 January.

DOI: 10.2514/6.2005-1301

Google Scholar

[12] Wohlers, T. (2006), Rapid prototyping and manufacturing state of the industry report, Annual Worldwide Progress Report, Wohlers Associate Inc., Fort Collins, CO.

Google Scholar

[13] Tyler, Charles. (2004) A Joint Computational Fluid Dynamics and Experimental Fluid Dynamics Test Program, AIAA Paper 2004-877, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January (2004).

DOI: 10.2514/6.2004-877

Google Scholar

[14] Jordan, J.D., et. al. (2003).

Google Scholar

[15] Hildebrand, Richard J., Eidson, Robert C., and Tyler, Charles. (2003), Development of a Low Cost, Rapid Prototype, Lambda-Wing/Body Wind Tunnel Model, AIAA Paper 2003-3818, 21st AIAA Applied Aerodynamics Conference, Orlando, FL, June (2003).

DOI: 10.2514/6.2003-3818

Google Scholar

[16] Tyler, Charles, Fonov, S.D., Goss, L.P., Jones, E.G., Crafton, J.W., and Sarka, B. Jr. (2004).

Google Scholar