[go: up one dir, main page]

Domb et al., 1998 - Google Patents

Modelling of stiffener crippling phenomena using finite element analysis

Domb et al., 1998

Document ID
8128570498894142038
Author
Domb M
Elliott W
Leigh B
Publication year
Publication venue
Canadian aeronautics and space journal

External Links

Continue reading at scholar.google.com (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06Frames; Stringers; Longerons; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06Frames; Stringers; Longerons; Fuselage sections
    • B64C1/12Construction or attachment of skin panels

Similar Documents

Publication Publication Date Title
Bordas et al. Enriched finite elements and level sets for damage tolerance assessment of complex structures
US7840389B2 (en) Method of optimizing stiffened panels under stress
Ovesy et al. Post-buckling analysis of delaminated composite laminates with multiple through-the-width delaminations using a novel layerwise theory
Bouazizi et al. Mechanical response of a hexagonal grid stiffened design of a pressurized cylindrical shell-application to aircraft fuselage
Sepe et al. Numerical and experimental investigation on the structural behaviour of a horizontal stabilizer under critical aerodynamic loading conditions
Zheng et al. Delamination interaction in laminated structures
Domb et al. Modelling of stiffener crippling phenomena using finite element analysis
Ivančević et al. Micromechanical damage modelling using a two-scale method for laminated composite structures
Van den Brink et al. Design for manufacturing of fuselage panels with curved grid stiffening
Wegner et al. Application of advanced grid-stiffened structures technology to the Minotaur payload fairing
Ambur et al. Design and evaluation of composite fuselage panels subjected to combined loading conditions
Azikov et al. Effective application of an anisogrid composite to design the components of the aircraft wing structure
Cecchini et al. Brazier effect in multibay airfoil sections
Tanaka et al. Buckling and collapse analysis of a cracked panel under a sequence of tensile to compressive load employing a shell-solid mixed finite element modeling
Yovanof et al. Advanced structural stability analysis of a non-circular, BWB-shaped vehicle
Shanygin et al. Multilevel approach for strength and weight analyses of composite airframe structures
Paroissien et al. Hybrid (bolted/bonded) joints applied to aeronautic parts: analytical one-dimensional models of a single-lap joint
Cosentino et al. Nonlinear analytical approach for preliminary sizing of discrete composite stringer terminations
Murphy et al. Efficient non-linear idealisations of aircraft fuselage panels in compression
Mert et al. Post-Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures
Starnes, H, Jr et al. Nonlinear response of damaged stiffened shells subjected to combined internal pressure and mechanical loads
Muñoz et al. Detailed FE aircraft fuselage sections for water impact simulations in the pre-design process chain
Kopecki et al. Modeling problems of the post-critical states of deformation of isogrid plates in the light of the preliminary experimental investigations
Knight Jr et al. Computational structural mechanics: A new activity at the NASA Langley Research Center
Kordas et al. Numerical Investigation of an Experimental Setup for Thermoplastic Fuselage Panel Testing in Combined Loading