Author: William L. KoPublisher:
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. KoPublisher:
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. KoPublisher:
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 Adm NasaPublisher: Independently Published
ISBN: 9781729195260
Category : Science
Languages : en
Pages : 32
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: NASA Technical Memorandum
Author: Mechanical and Thermal Buckling Analysis of Rectangular Sandwich Panels Under Different Edge Conditions
Author: William L. KoPublisher:
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. KoPublisher:
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. KoPublisher:
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. KoPublisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Author: