Full-Scale Testing and Analysis of Curved Aircraft Fuselage Panels.

Samavedam, Gopal; Hoadley, D.; Thompson, D.; Foster-Miller Associates; John A. Volpe National Transportation Systems Center (U.S.)

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Full-Scale Testing and Analysis of Curved Aircraft Fuselage Panels.

1993-12-01
By Samavedam, Gopal ; Hoadley, D. ; Thompson, D.

[PDF-3.05 MB]

English

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Details:

Creators:

Samavedam, Gopal ; Hoadley, D. ; Thompson, D.

Samavedam, Gopal ; Hoadley, D. ; Thompson, D. Less -
Corporate Creators:

Foster-Miller Associates ; John A. Volpe National Transportation Systems Center (U.S.)

Foster-Miller Associates ; John A. Volpe National Transportation Systems Center (U.S.) Less -
Subject/TRT Terms:

[+]

Aging Aircraft Airframes Cracking Fatigue Fatigue (Mechanics) Fuselage Fracture Fuselages Lap Splice Maintenance Multiple-site Damage Residual Strength
Publication/ Report Number:

DOT-VNTSC-FAA-93-10 ; DOT-FAA-CT-93-78

DOT-VNTSC-FAA-93-10 ; DOT-FAA-CT-93-78 Less -
Resource Type:

Tech Report
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

The report presents data on (1) residual strength of aircraft panels containing Multiple-Site Damage (MSD) in lap splices, and (2) fatigue strength of panels subjected to cyclic pressure loading. The testing was conducted using the dedicated Aging Aircraft Test Facility previously built in the Foster-Miller laboratory. A previous report describes the work in the first phase involving the design and operation of the facility and the test data generated on residual strength of panels with longitudinal midday skin cracks.
Content Notes:

Introduction, Test program, Panel design, Panel residual strength tests, Panel fatigue test, Conclusions and recommendations, References
Format:

PDF
Collection(s):

Volpe Center
Main Document Checksum:

[+]

urn:sha256:312d9e07467ef803c05bd2375e8c44d18534f917a5103c8ecfa0d18fa4c5f529
Download URL:

https://rosap.ntl.bts.gov/view/dot/9440/dot_9440_DS1.pdf
File Type:

No Additional Files

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Full-Scale Testing and Analysis of Curved Aircraft Fuselage Panels.

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