Bonded Repairs of Composite Panels Representative of Wing Structure-Reference-Cited by-同舟云学术

Bonded Repairs of Composite Panels Representative of Wing Structure

Published:2019-07-03 Issue: Volume: Page:565-580
ISSN:2195-4356
Container-title:ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing
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Author:

Bakuckas John G.,Chadha Reewanshu,Swindell Paul,Fleming Michael,Lin John Z.,Ihn J. B.,Desai Nihar,Espinar-Mick Erick,Freisthler Mark

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-030-21503-3_45

Reference3 articles.

1. Baker, A.A., Rose, L.R.F., Jones, R. (eds.).: Advances in the Bonded Composite Repair of Metallic Aircraft Structure, vols. 1 and 2. Elsevier, Amsterdam (2002)

2. Federal Aviation Adminsitration.: Bonded repair size limits. FAA Policy Statement, U.S. Department of Transportation, Federal Aviation Administration, Policy No. PS-AIR-100-14-130-001, Initiated By: AIR-100 (2014)

3. Chadha, R., Bakuckas, J., Fleming, M., Lin, J., Korkosz, G.: Airframe Beam Structural Test (ABST) fixture - capabilities description and user manual. DOT/FAA/TC-TN19/7 (2019)

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