Comparison of Swept-Frequency Transfer Function and Pulse Testing of a Full-Scale Graphite Wingbox Test Article to Support Lightning Indirect Effects Analysis

Document Number: 2001-01-2915

Date Published: September 2001

Author(s):
Mike Dosch - Boeing Commercial Airplanes
Joe Heeter - Boeing Commercial Airplanes
Barbara Melander - Boeing Commercial Airplanes

Abstract:
This paper reports some of the results of a NASA- prototype composite wingbox direct drive test, performed in the Boeing Lightning Lab from October 23, 2000 to June 8, 2001. The test data is being used to support computer analysis program and modeling efforts that are researching issues concerned with composite fuel tank designs.

File Size: 125K
Product Status: In Stock

See other papers presented at International Conference on Lightning and Static Electricity, September 2001, Seattle, WA, USA, Session: Lightning Indirect Effects Certification Issues

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