This paper is about shock wave propagation inside an aircraft fuselage, caused either by a terrorist device or by an accidental explosion. The concern over blasts inside airframes, stemming from past terrorist attacks on commercial aviation using concealed explosives, continues unabated and extends to luggage, passengers, and air cargo. In earlier publications by the present authors, it was noted that all previous aviation security studies lacked optical shock imaging, the principal tool of explosion and shock wave research. In an effort to correct this, high-speed schlieren shock wave cinematography methods on a large scale are demonstrated here for aircraft hardening studies. This capability is used to examine shock propagation in realistic aircraft interior scenarios, as well as to carry out some basic experiments toward an improved understanding of internal blast wave behavior.
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ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference
July 6–10, 2003
Honolulu, Hawaii, USA
Conference Sponsors:
- Fluids Engineering Division
ISBN:
0-7918-3697-5
PROCEEDINGS PAPER
Optical Shock Wave Imaging for Aviation Security
Gary S. Settles,
Gary S. Settles
Pennsylvania State University, University Park, PA
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Jeremy R. Benwood,
Jeremy R. Benwood
Pennsylvania State University, University Park, PA
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Joseph A. Gatto
Joseph A. Gatto
Transportation Security Laboratory, Atlantic City, NJ
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Gary S. Settles
Pennsylvania State University, University Park, PA
Jeremy R. Benwood
Pennsylvania State University, University Park, PA
Joseph A. Gatto
Transportation Security Laboratory, Atlantic City, NJ
Paper No:
FEDSM2003-45606, pp. 113-118; 6 pages
Published Online:
February 4, 2009
Citation
Settles, GS, Benwood, JR, & Gatto, JA. "Optical Shock Wave Imaging for Aviation Security." Proceedings of the ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. Volume 2: Symposia, Parts A, B, and C. Honolulu, Hawaii, USA. July 6–10, 2003. pp. 113-118. ASME. https://doi.org/10.1115/FEDSM2003-45606
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