Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments

Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments PDF Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32

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Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments

Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments PDF Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32

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Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments

Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments PDF Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32

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Combined-Load Buckling Behavior of Metal-Matrix Composite Sandwich Panels Under Different Thermal Environments

Combined-Load Buckling Behavior of Metal-Matrix Composite Sandwich Panels Under Different Thermal Environments PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722104290
Category :
Languages : en
Pages : 30

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Combined compressive and shear buckling analysis was conducted on flat rectangular sandwich panels with the consideration of transverse shear effects of the core. The sandwich panel is fabricated with titanium honeycomb core and laminated metal matrix composite face sheets. The results show that the square panel has the highest combined load buckling strength, and that the buckling strength decreases sharply with the increases of both temperature and panel aspect ratio. The effect of layup (fiber orientation) on the buckling strength of the panels was studied in detail. The metal matrix composite sandwich panel was much more efficient than the sandwich panel with nonreinforced face sheets and had the same specific weight. Ko, William L. and Jackson, Raymond H. Armstrong Flight Research Center RTOP 532-09-01...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296

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Mechanical and Thermal Buckling Analysis of Rectangular Sandwich Panels Under Different Edge Conditions

Mechanical and Thermal Buckling Analysis of Rectangular Sandwich Panels Under Different Edge Conditions PDF Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 80

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Predictions of Thermal Buckling Strengths of Hypersonic Aircraft Sandwich Panels Using Minimum Potential Energy and Finite Element Methods

Predictions of Thermal Buckling Strengths of Hypersonic Aircraft Sandwich Panels Using Minimum Potential Energy and Finite Element Methods PDF Author: William L. Ko
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 64

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Compressive and Shear Buckling Analysis of Metal Matrix Composite Sandwich Panels Under Different Thermal Environments

Compressive and Shear Buckling Analysis of Metal Matrix Composite Sandwich Panels Under Different Thermal Environments PDF Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28

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Thermostructural Behavior of a Hypersonic Aircraft Sandwich Panel Subjected to Heating on One Side

Thermostructural Behavior of a Hypersonic Aircraft Sandwich Panel Subjected to Heating on One Side PDF Author: William L. Ko
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

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