Thermal-Structural Analysis of Ni-Based Alloy Panel with Active Cooling Thermal Protection System

Guo Sun; Yuan Gui Sun

doi:10.4028/www.scientific.net/AMM.644-650.4718

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Finite Element Analysis of Stiffened Composite Panels Subjected by Low-Velocity Impact
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Thermal-Structural Analysis of Ni-Based Alloy...

Thermal-Structural Analysis of Ni-Based Alloy Panel with Active Cooling Thermal Protection System

Abstract:

In hypersonic environments, the development of aircraft engine presents the mitigation of the extreme thermal environment inside the combustion chamber. This paper establishes the capabilities for combustor panel design. By given the key loading and boundary conditions of the panel structure, the thermal structural analysis determines temperatures and stresses and the optimization improves panel’s robustness subject to thermal mechanical loads. A parametric sweep analysis is carried and the results give the optimal value of the panel face thickness.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

4718-4721

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.4718

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Online since:

September 2014

Authors:

Guo Sun*, Yuan Gui Sun

Keywords:

Active Cooling, Optimization, Thermal Protection, Thermal Structural Analysis

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