Thermally Induced Stresses Due to Coefficient of Thermal Expansion Mismatch in Hybrid Metallic/Composite Structures

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Thermally Induced Stresses Due to Coefficient of Thermal Expansion Mismatch in Hybrid Metallic/Composite Structures

2017-01-01

File Language:

English

Details

Publication/ Report Number:

DOT/FAA/TC-TN17/41
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:sha256:740d3319f079449f8d3b72949413ad9c7d0471e7625ca5764b6f6eefa706037e
Download URL:

https://rosap.ntl.bts.gov/view/dot/57866/dot_57866_DS1.pdf
File Type:

[PDF - 175.74 KB ]

File Language:

English

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Details

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