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Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 57.

through the interior spaces of the hull. The propagation of explosive shock waves and Supersonic gas flows within multiple, interlinking, cavities having indeterminate energy absorption and reflection properties, and ill-defined structural response, is extremely complex.
Open official document at PDF page 57AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page 53. PDF page 61.

reflected in such a way as produce shock loading on a localised area of the pressure hull. Supersonic gas flows The gas produced by the explosive would have resulted in a supersonic flow of very high pressure gas through the
Open official document at PDF page 61AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie