Author: William L. KoPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 20
Book Description
Mechanical and Thermal Buckling Analysis of Sandwich Panels Under Different Edge Conditions
Author: William L. KoPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 20
Book Description
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: Publisher: DIANE Publishing
ISBN: 1422348814
Category :
Languages : en
Pages : 54
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1096
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 712
Book Description
Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission
Author: William L. KoPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 46
Book Description
Heat transfer, thermal stresses, and thermal buckling analyses were performed on the unconventional wing structures of a Hyper-X hypersonic flight research vehicle (designated as X-43) subject to nominal Mach 7 aerodynamic heating. A wing midspan cross was selected for the the heat transfer and thermal stress analyses. Thermal buckling analysis was performed on three regions of the wing skin (lower or upper); 1) a fore wing panel, 2) an aft wing panel, and 3) a unit panel at the middle of the aft wing panel. A fourth thermal buckling analysis was performed on a midspan wing segment. The unit panel region is identified as the potential thermal buckling initiation zone. Therefore, thermal buckling analysis of the Hyper-X wing panels could be reduced to the thermal buckling analysis of that unit panel. "Buckling temperature magnification factors" were established. Structural temperature-time histories are presented. The results show that the concerns of shear failure at wing and spar welded sites.
Scientific and Technical Aerospace Reports
Author: Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638
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: