Führer et al., 2016 - Google Patents
Automated model generation and sizing of aircraft structuresFührer 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 …
- 238000004513 sizing 0 title abstract description 38
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5095—Vehicle design, e.g. aircraft or automotive design
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5086—Mechanical design, e.g. parametric or variational design
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/02—Component-based CAD
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/44—Composites
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/06—Constraint-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 |