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

Date Published: 2001-09-11

Paper Number: 2001-01-2915

DOI: 10.4271/2001-01-2915

Citation:

Dosch, M., Heeter, J., and Melander, B., "Comparison of Swept-Frequency Transfer Function and Pulse Testing of a Full Scale Graphite Wingbox Test Article to Support Lightning Indirect Effects Analysis," SAE Technical Paper 2001-01-2915, 2001, doi:10.4271/2001-01-2915.

Author(s):

Mike Dosch - The Boeing Co., Phantom Works
Joe Heeter - The Boeing Co., Phantom Works
Barbara Melander - The Boeing Co., Phantom Works

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 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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