Author:
Publisher: DIANE Publishing
ISBN: 1422348814
Category :
Languages : en
Pages : 54
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
Publisher: DIANE Publishing
ISBN: 1422348814
Category :
Languages : en
Pages : 54
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
Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission
Author: William L. Ko
Publisher:
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.
Publisher:
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.
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
Government Reports Announcements & Index
Mechanical Engineering
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 930
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 930
Book Description
Applied Mechanics Reviews
International Aerospace Abstracts
Aircraft Structures for Engineering Students
Author: Thomas Henry Gordon Megson
Publisher: Hodder Education
ISBN: 9780713136814
Category : Aeroelasticity
Languages : en
Pages : 0
Book Description
This book provides a self-contained course in aircraft structures which contains not only the fundamentals of elasticity and aircraft structural analysis but also the associated topics of airworthiness and aeroelasticity.
Publisher: Hodder Education
ISBN: 9780713136814
Category : Aeroelasticity
Languages : en
Pages : 0
Book Description
This book provides a self-contained course in aircraft structures which contains not only the fundamentals of elasticity and aircraft structural analysis but also the associated topics of airworthiness and aeroelasticity.
Analysis and Design of Flight Vehicle Structures
Author: Elmer Franklin Bruhn
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008
Book Description
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008
Book Description