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Characterisation of the realistic impact threat from runway debris

Published online by Cambridge University Press:  04 July 2016

E. S. Greenhalgh ,
G. A. F. Chichester ,
A. Mew ,
M. Slade  and
R. Bowen
E. S. Greenhalgh
Affiliation:
Structures and Materials Centre, QinetiQ Farnborough, UK
G. A. F. Chichester
Affiliation:
Structures and Materials Centre, QinetiQ Farnborough, UK
A. Mew
Affiliation:
Structures and Materials Centre, QinetiQ Farnborough, UK
M. Slade
Affiliation:
Structures and Materials Centre, QinetiQ Farnborough, UK
R. Bowen
Affiliation:
NDE Centre, Department of Mechanical Engineering, University College, London
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Abstract

This paper describes a study to characterise the impact threat to aircraft from runway debris. This work investigated the likelihood of an event exceeding a critical impact energy; it did not address the probability of an event occurring. Runway debris was collected from six airfields and parameters such as size fraction, mass, density, bluntness and material type were characterised. The distribution of the stone mass against frequency was accurately modelled and based on this, an expression was developed for the probability of an impact exceeding a critical level during a single take-off or landing. By considering the probability of a 50J impact from runway debris as a once in a lifetime event, the implication is that the actual threat is significantly more than the currently perceived threat. This study provides the foundations for more comprehensive studies and will give the designers improved understanding of the threat to aircraft from runway debris.

Type
Research Article
Information
The Aeronautical Journal , Volume 105 , Issue 1052 , October 2001 , pp. 557 - 570
Copyright
Copyright © Royal Aeronautical Society 2001 

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References

1. Bowen, R., Bleay, S., Greenhalgh, E., Lord, S., Mew, A. and Willows, M. A critical review of impact tolerance standards for composite materials, 1998, DERA/MSS/CR980550/I.0.Google Scholar
2. Ireman, T. Efficient design and verification of composite structures (EDAVCOS), Proposal for the programme on RTD industrial and materials technologies, 1997, Area 3A, Proposal Description part Bl and B2.Google Scholar
3. Olsson, R. Mass criterion for wave controlled impact responses of composite plates, 2000, Composites Part A, 31, pp 879–887.Google Scholar
4. Sierakowski, R. and Chaturvedi, S. Impact loading in filamentary structural composites, 1983, Shock and Vibration Digest, 15, (10), pp 13–31.Google Scholar
5. Kumar, P. and Rai, B. Delaminations of barely visible impact damage in CFRP laminates, 1993, Composite Structures, 23, pp 313–318.Google Scholar
6. Wurzel, D.Design,fabricationandqualificationof composite carbon/epoxy horizontal stabilizer components, 1983, 9th Annual Mini- Symposium on Aerospace Science and Technology, Wright-Patterson AFB.Google Scholar
7. Frazier, J. and Clemons, A. Evaluation of the thermoplastic film interleaf concept for improved damage tolerance, 1990, 35th Int SAMPE Symp and Exhib, Anaheim, CA, 2-9 April.Google Scholar
8. Hosur, M., Murthy, C. and Ramurthy, T. Compression after impact testing of carbon-fibre reinforced plastic laminates, 1999, J of Compos ites Tech and Research, 21, (2), pp 51–64.Google Scholar
9. Adsit, N. and Waszczak, J. Effect of near visual damage on the properties of graphite/epoxy, 1979, Composite Materials; Testing & Design, ASTM STP674.Google Scholar
10. Olsson, R. Damocles Task 1 — Deliverable: A survey of impact conditions relevant in aircraft composite structures,1998, FFAP H-1353, FFA — The Aeronautical Research Institute of Sweden.Google Scholar
11. Olsson, R. Experimental verification of a theory for the impact response of composite plates, 1991, FFA TN 1991-17, FFA — The Aeronautical Research Institute of Sweden.Google Scholar
12. Cantwell, W. and Morton, J. The influence of varying projectile mass on the impact response of CFRP, 1989, Composite Structures, 13, pp 101–114.Google Scholar
13. Greenhaloh, E., Chichester, G., Mew, A. and Slade, M. Characterisation of the realistic impact threat from runway debris, 2000, DERA Technical Report DERA/MSS/MSMA2/TR000702.Google Scholar
14. http://www.raf.mod.uk/rafhome.html Google Scholar
15. Bevington, P. and Robinson, K. Data Reduction and Error Analysis for the. Physical Sciences, 1992, Mcgraw-Hill, 2nd Ed, ISBN 0 07 911243 9.Google Scholar
16. Cooper, M. QBE International, 2000, Private communication.Google Scholar
17. Olsson, R. Impact response of composite laminates — A guide to closed form solutions, 1992, FFA TN 1992-33, FFA — The Aeronautical Research Institute of Sweden.Google Scholar
18. Schumann, W. Collins Photo Guide; Rocks, Minerals and Gemstones, 1999, Harper-Collins, ISBM 0002199092.Google Scholar
19. Osborne, N. and Gawes, G. LANTIRN Infrared Window Failure Analysis,1994,Proceedingsof theInt ConferenceonInfrared Windows & Domes, San Diego, CA, pp 444-455.Google Scholar
20. Moon, J. DERA, 2000, Private communication.Google Scholar