Add to ORKGIssued as Final technical report, Project no. E-20-671Final technical report has title: Structural integrity of aging airplane
PDFTech Reporthttp://adsabs.harvard.edu/abs/1994asim.nasa...85BAircraft structural componentsCrackin...
Early airplanes were designed using purely static conditions and mainly tested only based on simple ...
International technical experts in durability and damage tolerance of metallic airframe structures w...
Aircraft structural integrity management programs are aimed at ensuring that aircraft can operate sa...
Abstract--Integrity evaluation of aging structures i extremely important to ensure economic and safe...
00860481https://doi.org/10.21949/14037921996PDFTech ReportDOT/FAA/AR-95/47Civil aviationFuselagesAir...
Structural integrity assessment of aging flight vehicles is extremely important to ensure their econ...
29950519PDFTech ReportDOT-VNTSC-FAA-93-08DOT-FAA-CT-94-10Fatigue (Mechanics)Fracture testsFuselagesC...
29774853PDFTech ReportDOT-VNTSC-FAA-93-11DOT-FAA-CT-93-79FuselagesAirframesFatigue (Mechanics)Mainte...
This paper presents a methodology for predicting the thresholds of multiple site damage and widespre...
29786115PDFTech ReportDOT-VNTSC-FAA-93-10DOT-FAA-CT-93-78AirframesFuselagesCrackingFatigue (Mechanic...
A numerical study is presented of the residual strength of an aircraft fuselage in the presence of m...
NASA is developing a 'tool box' that includes a number of advanced structural analysis computer code...
The problem of multiple site damage in aged airplane fuselage is handled in this paper. The analytic...
https://doi.org/10.21949/14045911997PDFProceedingshttp://www.tc.faa.gov/its/worldpac/techrpt/ar97-2-...
PDFTech Reporthttp://adsabs.harvard.edu/abs/1994asim.nasa...85BAircraft structural componentsCrackin...
Early airplanes were designed using purely static conditions and mainly tested only based on simple ...
International technical experts in durability and damage tolerance of metallic airframe structures w...
Aircraft structural integrity management programs are aimed at ensuring that aircraft can operate sa...
Abstract--Integrity evaluation of aging structures i extremely important to ensure economic and safe...
00860481https://doi.org/10.21949/14037921996PDFTech ReportDOT/FAA/AR-95/47Civil aviationFuselagesAir...
Structural integrity assessment of aging flight vehicles is extremely important to ensure their econ...
29950519PDFTech ReportDOT-VNTSC-FAA-93-08DOT-FAA-CT-94-10Fatigue (Mechanics)Fracture testsFuselagesC...
29774853PDFTech ReportDOT-VNTSC-FAA-93-11DOT-FAA-CT-93-79FuselagesAirframesFatigue (Mechanics)Mainte...
This paper presents a methodology for predicting the thresholds of multiple site damage and widespre...
29786115PDFTech ReportDOT-VNTSC-FAA-93-10DOT-FAA-CT-93-78AirframesFuselagesCrackingFatigue (Mechanic...
A numerical study is presented of the residual strength of an aircraft fuselage in the presence of m...
NASA is developing a 'tool box' that includes a number of advanced structural analysis computer code...
The problem of multiple site damage in aged airplane fuselage is handled in this paper. The analytic...
https://doi.org/10.21949/14045911997PDFProceedingshttp://www.tc.faa.gov/its/worldpac/techrpt/ar97-2-...
PDFTech Reporthttp://adsabs.harvard.edu/abs/1994asim.nasa...85BAircraft structural componentsCrackin...
Early airplanes were designed using purely static conditions and mainly tested only based on simple ...
International technical experts in durability and damage tolerance of metallic airframe structures w...