Andere Kunden interessierten sich auch für
![Characterization of Functionally Graded Materials]( "Characterization of Functionally Graded Materials")
Characterization of Functionally Graded Materials63,99 €![An Exploration of Several Structural Measurement Techniques for Usage With Functionally Graded Materials]( "An Exploration of Several Structural Measurement Techniques for Usage With Functionally Graded Materials")
An Exploration of Several Structural Measurement Techniques for Usage With Functionally Graded Materials63,99 €![Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite]( "Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite")
Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite63,99 €![Mechanics of a Functionally-Graded Titanium Matrix Composite]( "Mechanics of a Functionally-Graded Titanium Matrix Composite")
Mechanics of a Functionally-Graded Titanium Matrix Composite63,99 €![Raman Fiber Lasers and Amplifiers Based on Multimode Graded-Index Fibers and Their Application to Beam Cleanup]( "Raman Fiber Lasers and Amplifiers Based on Multimode Graded-Index Fibers and Their Application to Beam Cleanup")
Raman Fiber Lasers and Amplifiers Based on Multimode Graded-Index Fibers and Their Application to Beam Cleanup63,99 €![Disruption in Space System Design: Exploiting Carbon Nanotubes in Structures and Component Materials in 2030]( "Disruption in Space System Design: Exploiting Carbon Nanotubes in Structures and Component Materials in 2030")
Disruption in Space System Design: Exploiting Carbon Nanotubes in Structures and Component Materials in 203063,99 €![Crack Turning in Integrally Stiffened Aircraft Structures]( "Crack Turning in Integrally Stiffened Aircraft Structures")
Crack Turning in Integrally Stiffened Aircraft Structures63,99 €
A Functionally Graded Material (FGM) is a material which has a continuous variation of material properties through-the-thickness. This thesis will explore analysis of FGM flat plates and shell panels, and use FGM's unique characteristics to retrofit a cracked exhaust wash structure. FGMs are first characterized as flat plates under pressure and thermal loading. Next, FGM shell panels are characterized under thermal loading. Conclusions drawn from FGM characterization are used to develop a patch to retrofit a cracked aircraft exhaust wash structure. The exhaust wash structure is first analyzed to provide a baseline and then several FGM patches are evaluated on their ability to reduce stress and deflection. Finally, an exhaust wash panel made of FGM is analyzed.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.