Hostname: page-component-586b7cd67f-g8jcs Total loading time: 0 Render date: 2024-11-29T02:07:10.106Z Has data issue: false hasContentIssue false
  • English
  • Français

The role of modelling and simulation in the development of advanced non-destructive evaluation systems

Published online by Cambridge University Press:  04 July 2016

E. R. Generazio  and
C. E. Harris
E. R. Generazio
Affiliation:
National Aeronautics and Space Administration, Langley Research Center, Hampton, USA
C. E. Harris
Affiliation:
National Aeronautics and Space Administration, Langley Research Center, Hampton, USA
Get access Rights & Permissions [Opens in a new window]

Abstract

Non-destructive evaluation (NDE) technologies are a critical component of a collaborative engineering environment. The role of NDE simulations in component design, manufacturing, certification, integrity and repair are identified and discussed in the context of a futuristic intelligent synthesis environment (ISE) that facilitates collaborative engineering. Each of these critical areas needs to be simulated in a virtual reality environment and is expected to have a large effect on the cost, life, safety, and risk of aerospace products. In a collaborative engineering environment, NDE simulations will provide ‘real-time’ feedback to component designers and systems engineers. This feedback is necessary to achieve optimum overall system-level benefits.

Type
Research Article
Information
The Aeronautical Journal , Volume 103 , Issue 1025 , July 1999 , pp. 325 - 328
Copyright
Copyright © Royal Aeronautical Society 1999 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Generazio, E.R., Chamis, C.C. and Abumeri, G. Technology Benefit Estimator (T/T3EST) — User's Manual, NASA TM-106785, National Aeronautics and Space Administration, Washington, DC, 20546, December 1994.Google Scholar
2. Generazio, E.R. and Chamis, C.C. Technology benefit estimator for aerospace propulsion systems, AIAA-94-3096, 27-29 June 1994, pp 1–14.Google Scholar
3. Nemeth, N.N., Powers, L.M., Janosik, L.A. and Gyekenyesi, J.P. Designing ceramic components for durability, American Ceramic Society Bulletin, December 1993, 72, (12), pp 59–69.Google Scholar
4. Nemeth, N.N., Powers, L.M., Janosik, L.A. and Gyekenyesi, J.P. Durability evaluation of ceramic components using CARES/Life, ASME J Eng for Gas Turbines and Power, January 1996, 118, (1), pp 150–158.Google Scholar
5. Conley, J., Moran, B. and Gray, J. Aluminum in automotive applications, SP1305, #980455, SAE, Warrendale, Pa, 1998, pp 25–38.Google Scholar
6. Elshafiey, I. and Gray, J. Optimization tool for X-Ray radiography NDE, Review of Progress in Quantitative NDE, 15A, Thompson, D.O. and Chimenti, D.E. (Eds), Plenum Press, New York, NY, 1996, pp 425–432.Google Scholar
7. Gray, T.A. Ultrasonic inspectability models for jet engine forgings, In: Review of Progress in Quantitative Non-destructive Evaluation, 17, D.O., Thompson and Chimenti, D.E. (Eds), Plenum Press, New York, 1998, pp 2053–2060.Google Scholar
8. Syed, H.I., Winfree, W.P., Cramer, K.E. and Howell, P.A. Thermographic detection of corrosion in aircraft skin, Review of Progress in Quantitative Non-destructive Evaluation, 12B, Thompson, D.O. and Chimenti, D.E. (Eds), 1993, pp 2035–2041.Google Scholar
9. Emeric, P.R. and Winfree, W.P. Thermal characterization of multilayer structures from transient thermal response, Review of Progress in Quantitative Non-destructive Evaluation, 13B, Thompson, D.O. and Chimenti, D.E. (Eds), 1994, pp 1963–1970.Google Scholar