A Quasi-Statistical Approach to Aircraft Induced Effects Characterisation

Format:

Conference/Event

Author/Creator:

Jones, C. C. R., author.

Conference Name:

International Conference on Lightning and Static Electricity (2001-09-11 : Seattle, Washington, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2001

Summary:

In order to demonstrate comprehensively for every cable to every flight safety critical equipment on an aircraft, that the qualification test levels were greater by a margin than the levels of induced threat on the aircraft, it is necessary to measure the current or voltage on all of those cables during whole aircraft tests. In this paper an approach is described which relies on a statistical distribution of induced threat amplitudes in the cables within an airframe to reduce the number of cable measurements needed, and fill in for cables that cannot be measured. The method also offers, for the first time, a viable approach to the substantiation of a similarity argument

Notes:

Vendor supplied data

Publisher Number:

2001-01-2918

Access Restriction:

Restricted for use by site license