Han et al., 2010 - Google Patents
A variable-fidelity modeling method for aero-loads predictionHan et al., 2010
View PDF- Document ID
- 10206862087412970210
- Author
- Han Z
- Görtz S
- Hain R
- Publication year
- Publication venue
- New Results in Numerical and Experimental Fluid Mechanics VII: Contributions to the 16th STAB/DGLR Symposium Aachen, Germany 2008
External Links
Snippet
Summary A Variable-Fidelity Modeling (VFM) method has been developed as an efficient and accurate aerodynamic data modeling strategy. In this approach, a set of CFD methods with varying degrees of fidelity and computational expense is exercised to reduce the …
- 238000005070 sampling 0 abstract description 4
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
- 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
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/10—Complex mathematical operations
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Han et al. | A variable-fidelity modeling method for aero-loads prediction | |
| CN112016167B (en) | Aircraft aerodynamic shape design method and system based on simulation and optimization coupling | |
| CN105843073B (en) | A kind of wing structure aeroelastic stability analysis method not knowing depression of order based on aerodynamic force | |
| CN106650046B (en) | A kind of unsteady characteristic acquisition methods in Ship Air flow field | |
| CN105975645B (en) | A kind of aircraft flow field of region containing shock wave quick calculation method based on multistep | |
| Rogers et al. | CFD simulations of the space launch system ascent aerodynamics and booster separation | |
| Rumpfkeil et al. | Multi-fidelity surrogate models for flutter database generation | |
| White et al. | Neural networks predict fluid dynamics solutions from tiny datasets | |
| CN109726433A (en) | The three-dimensional method for numerical simulation streamed without viscous low speed based on surface boundary condition | |
| CN116628854A (en) | Wing section aerodynamic characteristic prediction method, system, electronic equipment and storage medium | |
| CN106650028A (en) | Optimization method and system based on agile satellite design parameters | |
| Jung et al. | Low Reynolds number airfoil design for a mars exploration airplane using a transition model | |
| Díaz-Casás et al. | Wind turbine design through evolutionary algorithms based on surrogate CFD methods | |
| Dean et al. | Aircraft stability and control characteristics determined by system identification of CFD simulations | |
| CN110083946A (en) | A kind of modified method of multistate model based on unconstrained optimization model | |
| Volpiani et al. | Simulating the Common Research Model using the new CFD software from ONERA, DLR and Airbus | |
| CN110909511B (en) | Non-viscous low-speed streaming numerical simulation method without curved surface volume division | |
| Tancred et al. | Aerodynamic response quantification of complex hypersonic configurations using variable fidelity surrogate modeling | |
| Mehta et al. | Surrogate based design optimization of aerostat envelope | |
| Cameron et al. | Metamodel assisted multi-objective global optimisation of natural laminar flow aerofoils | |
| Sinha et al. | Reduced-order modeling of steady aerodynamics for 2D store separation analysis | |
| Anusonti-Inthra | Data-Driven Modeling of Aerodynamic Loadings for Tiltrotor Pylon using Multi-Fidelity CFD Data | |
| Rossow et al. | European numerical aerodynamics simulation systems | |
| Abu-Zurayk et al. | Development of the adjoint approach for aeroelastic wing optimization | |
| CN118551667B (en) | High-fidelity modeling method, device, equipment, medium and product |