Adhesively Bonded Repairs to Metallic Fuselage Structure: Test 4, Effect of Temperature and Humidity on Mechanical and Fatigue Behavior

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Adhesively Bonded Repairs to Metallic Fuselage Structure: Test 4, Effect of Temperature and Humidity on Mechanical and Fatigue Behavior

2019-01-01

File Language:

English

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Publication/ Report Number:

DOT/FAA/TC-19/21
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Format:

PDF
Collection(s):

FAA Technical Library
Main Document Checksum:

urn:sha256:54a13e7afe4e12ee1adf4871c6938a1461879b632a56f21616b88789fdb606a9
Download URL:

https://rosap.ntl.bts.gov/view/dot/57790/dot_57790_DS1.pdf
File Type:

[PDF - 34.62 MB ]

File Language:

English

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