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Filtering by: Subject Airplanes -- Materials Remove constraint Subject: Airplanes -- Materials Degree Field Mechanical Engineering Remove constraint Degree Field: Mechanical Engineering Non-Academic Affiliation Oregon State University. Graduate School Remove constraint Non-Academic Affiliation: Oregon State University. Graduate School

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Residual strength properties of Gr/BMI composite laminates after constant/cyclic compression

Creator:

Shenoy, Krishnananda

Resource Type:

Masters Thesis

Full Text:

would like to specially extend my appreciation to the Boeing Commercial Airplane Group for financing
An experimental approach to analyze large notched composite panels loaded in out-of-plane shear

Creator:

Froemming, Tyler M.

Abstract:

Identifying material characteristics of composites is important in designing any structural system. The aerospace industry relies on these material properties not only to design a functional aircraft, but also a safe and reliable one. Since carbon fiber composites are relatively new materials, little is known about its characteristics under certain...

Resource Type:

Masters Thesis

Full Text:

: _______________________________________________________________________ Brian K. Bay Identifying material characteristics of composites is important in
A force plate for measuring contact forces during dependent transfers onboard aircraft

Creator:

Schafer, Christopher A.

Abstract:

The transfer of air travelers with disabilities between a mobility aid and an aircraft seat is a major source of injury for both the travelers and the airline personnel assisting in the transfer. The risk to both parties might be reduced through the biomechanical study of the transfer task. Such...

Resource Type:

Masters Thesis
A nonlocal damage theory for laminated plate with application to aircraft damage tolerance

Creator:

Nahan, Matthew F.

Abstract:

Design of commercial aircraft structure, composed of composite material, requires the prediction of failure loads given large scale damage. In particular, a fuselage of graphite/epoxy lamination was analyzed for damage tolerance given a standard large crack that severed both skin and internal structure. Upon loading, a zone of damage is...

Resource Type:

Dissertation

Full Text:

: Timothy C. Kennedy Design of commercial aircraft structure, composed of composite material, requires the

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Academic Affiliation

Mechanical Engineering3
Mechanical, Industrial, and Manufacturing Engineering1

Advisor

Bay, Brian K.1
Kennedy, Timothy C.1
Wolff, Ernest G.1
Zaworski, Joseph R.1

Commencement Year

Commencement Year range begin – Commencement Year range end

Current results range from 1994 to 2014

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Committee Member

Albertani, Roberto1
Dietterich, Thomas1
Hoag, Stephen W.1
Kamke, Fred1
Kennedy, Timothy C.1
more Committee Members »

Creator

Froemming, Tyler M.1
Nahan, Matthew F.1
Schafer, Christopher A.1
Shenoy, Krishnananda1

Date

Date range begin – Date range end

Current results range from 1993 to 2013

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Decade

2010-20191
2000-20091
1990-19992

Degree Field

Mechanical Engineering[remove]4

Degree Level

Master's3
Doctoral1

Degree Name

Master of Science (M.S.)3
Doctor of Philosophy (Ph.D.)1

Language

English [eng]4

License

All rights reserved2

Non-Academic Affiliation

Oregon State University. Graduate School[remove]4

Peer Reviewed

No4

Resource Type

Masters Thesis3
Dissertation1

Rights Statement

Copyright Not Evaluated2
In Copyright2

Subject

Airplanes -- Materials -- Testing2
Airplanes -- Equipment and supplies -- Design and construction1
Airplanes -- Fuselage -- Testing1
Airplanes -- Seats -- Testing1
Carbon fibers -- Cracking1
more Subjects »

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