Nothing Special   »   [go: up one dir, main page]

Führer et al., 2016 - Google Patents

Automated model generation and sizing of aircraft structures

Führer et al., 2016

Document ID
3643017668400192299
Author
Führer T
Willberg C
Freund S
Heinecke F
Publication year
Publication venue
Aircraft Engineering and Aerospace Technology: An International Journal

External Links

Snippet

Purpose To obtain a good start configuration in the early design phase, simulation tools are used to create a large number of product designs and to evaluate their performance. To reduce the effort for the model generation, analysis and evaluation, a design environment for …
Continue reading at www.emerald.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
    • 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
    • G06F17/5095Vehicle design, e.g. aircraft or automotive design
    • 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
    • G06F17/5086Mechanical design, e.g. parametric or variational design
    • 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
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/02Component-based CAD
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/182Stringers, longerons
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/44Composites
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/06Constraint-based CAD

Similar Documents

Publication Publication Date Title
Brooks et al. Benchmark aerostructural models for the study of transonic aircraft wings
Brooks et al. Aerostructural tradeoffs for tow-steered composite wings
Gagnon et al. Aerodynamic optimization trade study of a box-wing aircraft configuration
Führer et al. Automated model generation and sizing of aircraft structures
Wunderlich et al. Global aerostructural design optimization of more flexible wings for commercial aircraft
US7406403B2 (en) Systems and methods for automatically generating 3D wireframe CAD models of aircraft
Iwaniuk et al. Multi-disciplinary optimisation approach for a light turboprop aircraft-engine integration and improvement
Goertz et al. Multi-level MDO of a long-range transport aircraft using a distributed analysis framework
Wunderlich et al. Multidisciplinary optimization of an NLF forward swept wing in combination with aeroelastic tailoring using CFRP: DLR contribution to the LuFo IV joint research project AeroStruct
Görtz et al. Collaborative multi-level MDO process development and application to long-range transport aircraft
Scherer et al. Fuselage structures within the CPACS data format
Keye et al. Aero-structural optimization of the NASA common research model
Chau et al. Fuel burn evaluation of a transonic strut-braced-wing regional aircraft through multipoint aerodynamic optimisation
Wunderlich et al. Global aero-structural design optimization of composite wings with active manoeuvre load alleviation
Schwinn et al. A parametric aircraft fuselage model for preliminary sizing and crashworthiness applications
Wunderlich et al. Integrated process chain for aerostructural wing optimization and application to an NLF forward swept composite wing
Wunderlich et al. Aeroelastic tailoring of an NLF forward swept wing: DLR contribution to LuFo IV joint research project AeroStruct
Ciampa et al. Preliminary design for flexible aircraft in a collaborative environment
Lange et al. Digital multi-disciplinary design process for moveables at virtual product house
Corman et al. Estimating jig shape for an aircraft wing determined through aerodynamic shape optimization with rigid body assumptions
Banerjee et al. CATIA V5-based parametric aircraft geometry modeler
Travaglini et al. PyPAD: a multidisciplinary framework for preliminary airframe design
Sinha et al. A framework for the bi-level optimization of a generic transport aircraft fuselage using aeroelastic loads
Mainini et al. Multidisciplinary integrated framework for the optimal design of a jet aircraft wing
Bravo-Mosquera et al. Exploration of box-wing aircraft concept using high-fidelity aerodynamic shape optimization