Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments
Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Combined-load Buckling Behavior of Metal-matrix Composite Sandwich Panels Under Different Thermal Environments
Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Combined-Load Buckling Behavior of Metal-Matrix Composite Sandwich Panels Under Different Thermal Environments
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722104290
Category :
Languages : en
Pages : 30
Book Description
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...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722104290
Category :
Languages : en
Pages : 30
Book Description
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
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
Book Description
Mechanical and Thermal Buckling Analysis of Rectangular Sandwich Panels Under Different Edge Conditions
Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 80
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 80
Book Description
Predictions of Thermal Buckling Strengths of Hypersonic Aircraft Sandwich Panels Using Minimum Potential Energy and Finite Element Methods
Author: William L. Ko
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 64
Book Description
Compressive and Shear Buckling Analysis of Metal Matrix Composite Sandwich Panels Under Different Thermal Environments
Author: William L. Ko
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
Book Description
Thermostructural Behavior of a Hypersonic Aircraft Sandwich Panel Subjected to Heating on One Side
Author: William L. Ko
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
Book Description