Sensitivity Analysis and Numerical Simulation of

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Sensitivity Analysis and Numerical Simulation of

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dc.contributor.author Charoenpon, Attapon
dc.contributor.author H, Niramol
dc.contributor.author S, Sedthawatt
dc.date.accessioned 2563-08-28T06:04:03Z
dc.date.available 2563-08-28T06:04:03Z
dc.date.issued 2559
dc.identifier.uri http://hdl.handle.net/123456789/2021
dc.description บทความวิจัย en_US
dc.description.abstract This paper presents a prediction of fatigue life sensitivity of Rocket detent catch used on rocket launcher tube for proper design and specify maintenance cycle. Detent catch is subjected to large stress and strain in a short duration time in the operation. The basic fatigue model was developed to predict fatigue compare to the numerical analysis. Many geometric parameters of detent catch were considered to evaluate sensitivity of fatigue life via pareto chart.The result showed compromising value between analytic and simulation. The arm width of detent catch has the most effect to failure cycle while the other features have some significant effect. en_US
dc.description.sponsorship Defence Technology Institute en_US
dc.language.iso en en_US
dc.publisher Defence Technology Institute en_US
dc.relation.ispartofseries 5963;
dc.subject fatigue en_US
dc.subject sensitivity en_US
dc.subject detent en_US
dc.subject numerical en_US
dc.subject pareto en_US
dc.title Sensitivity Analysis and Numerical Simulation of en_US
dc.type Article en_US


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