Back to Results
First PageMeta Content
Engineering / Management / Survival analysis / Design for X / Damage tolerance / Reliability engineering / Air safety / Fatigue / Risk / Failure / Engineering statistics / Systems engineering


A Method for Reliability Assessment of Aircraft Structures Subject to Accidental Damage
Add to Reading List

Document Date: 2005-06-14 14:04:09


Open Document

File Size: 363,20 KB

Share Result on Facebook

City

Washington / DC / Seattle / Melbourne / Langley / Reliability / /

Company

Literature Review / Sandia National Laboratories / Swartz D. D. / The Boeing Company / /

Country

United States / Australia / /

Facility

University of Washington / American Institute of Aeronautics / Naval Aviation depot / Maritime Research Laboratory / /

IndustryTerm

statistical tools / airline maintenance facilities / impact energy / numerical data fitting tools / material systems / closedform solution / numerical analysis tools / inspection tools / metal structures / probabilistic impact energy criteria / aerospace / obtained using numerical data fitting tools / /

Organization

Federal Aviation Administration / Univ. of Washington / Commercial Aircraft Composite Repair Committee / American Institute of Aeronautics / FAA Center of Excellence / National Aeronautics and Space Administration / University of Washington / Seattle / Department of Aeronautics and Astronautics / Aeronautical and Maritime Research Laboratory / TP PT / /

Person

Cary K. Huang / Andrey Styuart / Hamid Razi / Cliff Chen / Narciso / /

Position

author / Graduate Research Assistant / Professor / inspector / Representative / /

ProvinceOrState

Virginia / Washington / /

TVStation

Kuen / /

Technology

thermography / PDF / /

SocialTag