Raveh, 2005 - Google Patents
Computational-fluid-dynamics-based aeroelastic analysis and structural design optimization—a researcher's perspectiveRaveh, 2005
- Document ID
- 3786325025034730385
- Author
- Raveh D
- Publication year
- Publication venue
- Computer Methods in Applied Mechanics and Engineering
External Links
Snippet
The paper discusses current approaches for the use of computational fluid dynamics in aeroelastic analyses and structural design optimization applications. Current methods for computational fluid dynamics-based static maneuver load analysis and flutter analysis are …
- 238000004458 analytical method 0 title abstract description 75
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
- G06F17/10—Complex mathematical operations
- G06F17/11—Complex mathematical operations for solving equations, e.g. nonlinear equations, general mathematical optimization problems
- G06F17/13—Differential equations
-
- 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
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/16—Numerical modeling
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/44—Composites
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/80—Technologies aiming to reduce green house gasses emissions common to all road transportation technologies
- Y02T10/82—Tools or systems for aerodynamic design
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Kamakoti et al. | Fluid–structure interaction for aeroelastic applications | |
| Johnson et al. | Thirty years of development and application of CFD at Boeing Commercial Airplanes, Seattle | |
| Nielsen et al. | Discrete adjoint-based design optimization of unsteady turbulent flows on dynamic unstructured grids | |
| Beran et al. | Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities | |
| CN104133933B (en) | Vehicle aeroelastic behavior analysis method under a kind of hypersonic aircraft thermal environment | |
| Jonsson et al. | Computational modeling of flutter constraint for high-fidelity aerostructural optimization | |
| Reist et al. | Cross validation of aerodynamic shape optimization methodologies for aircraft wing-body optimization | |
| Gray et al. | High-fidelity aerostructural optimization with a geometrically nonlinear flutter constraint | |
| US20240068903A1 (en) | Generation of cfd-based structurally independent aerodynamic influence coefficient matrix | |
| Ripepi et al. | Improved matrix fraction approximation of aerodynamic transfer matrices | |
| Raveh | Computational-fluid-dynamics-based aeroelastic analysis and structural design optimization—a researcher’s perspective | |
| Kennedy et al. | An adjoint-based derivative evaluation method for time-dependent aeroelastic optimization of flexible aircraft | |
| Ghoman et al. | Multifidelity, multistrategy, and multidisciplinary design optimization environment | |
| Morris et al. | Domain-element method for aerodynamic shape optimization applied to modern transport wing | |
| Jonsson et al. | Development of flutter constraints for high-fidelity aerostructural optimization | |
| Guo et al. | Aero-structural optimization of supersonic wing under thermal environment using adjoint-based optimization algorithm | |
| Raveh | CFD-based gust response analysis of free elastic aircraft | |
| Bekemeyer et al. | Reduced order transonic aeroelastic gust response simulation of large aircraft | |
| Krüger et al. | Aeroelastic effects in multibody dynamics | |
| Nielsen | Adjoint-based aerodynamic design of complex aerospace configurations | |
| Munk et al. | Aerothermoelastic structural topology optimisation for a hypersonic transport aircraft wing | |
| Raveh et al. | Structural optimization of flight vehicles with non-linear aerodynamic loads | |
| Zuo et al. | Efficient aeroelastic design optimization based on the discrete adjoint method | |
| Scharpenberg et al. | Considerations on an integral flight physics model with application to loads analysis | |
| Bekemeyer | Rapid Computational Aerodynamics for Aircraft Gust Response Analysis |