Cheng et al., 2013 - Google Patents
Thermal-structural response and low-cycle fatigue damage of channel wall nozzleCheng et al., 2013
View HTML- Document ID
- 15727505423090913937
- Author
- Cheng C
- Wang Y
- Liu Y
- Liu D
- Lu X
- Publication year
- Publication venue
- Chinese Journal of Aeronautics
External Links
Snippet
To investigate the thermo-mechanical response of channel wall nozzle under cyclic working loads, the finite volume fluid-thermal coupling calculation method and the finite element thermal-structural coupling analysis technique are applied. In combination with the material …
- 230000004044 response 0 title abstract description 18
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]
- G06F2217/41—Molding
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Willcox et al. | Solid rocket motor internal ballistics simulation using three-dimensional grain burnback | |
| Müller et al. | Large-eddy simulation of nitrogen injection at trans-and supercritical conditions | |
| Jiawen et al. | Thermal-structural analysis of regeneratively-cooled thrust chamber wall in reusable LOX/Methane rocket engines | |
| Chen et al. | Coupled heat transfer and thermo-mechanical behavior of hypersonic cylindrical leading edges | |
| Li et al. | Fluid–solid coupled simulation of the ignition transient of solid rocket motor | |
| Zhao et al. | Aeroelastic response of rocket nozzles to asymmetric thrust loading | |
| Benoit et al. | Cyclic behaviour of structures under thermomechanical loadings: application to exhaust manifolds | |
| Galindo et al. | Development and validation of a radial variable geometry turbine model for transient pulsating flow applications | |
| CN107895088A (en) | A kind of aeroengine combustor buring room life-span prediction method | |
| Poursaeidi et al. | Effects of emergency and fired shut down on transient thermal fatigue life of a gas turbine casing | |
| Kowollik et al. | 3D fluid–structure interaction analysis of a typical liquid rocket engine cycle based on a novel viscoplastic damage model | |
| Staroselsky et al. | Transient thermal analysis and viscoplastic damage model for life prediction of turbine components | |
| Beesley et al. | A novel simulation for the design of a low cycle fatigue experimental testing programme | |
| Kumar et al. | Three-dimensional thermo-mechanical simulations of heterogeneous solid propellants | |
| Di et al. | Thermo-structural analysis of regenerative cooling thrust chamber cylinder segment based on experimental data | |
| Cheng et al. | Thermal-structural response and low-cycle fatigue damage of channel wall nozzle | |
| Zhang et al. | Multiscale reduced-order modeling of a titanium skin panel subjected to thermomechanical loading | |
| Tinga et al. | Gas turbine combustor liner life assessment using a combined fluid/structural approach | |
| Ferraiuolo et al. | A comparative study of refined and simplified thermo-viscoplastic modeling of a thrust chamber with regenerative cooling | |
| Hayden et al. | Strain Response and Aerodynamic Damping of a Swirl Distortion Generator Using Computational Fluid Dynamics | |
| Yazdi | Flutter of delaminated cross-ply laminated cylindrical shells | |
| Jiang et al. | Predicting the influence of overload and loading mode on fatigue crack growth: a numerical approach using irreversible cohesive elements | |
| Jiawen et al. | Damage localization effects of the regeneratively-cooled thrust chamber wall in LOX/methane rocket engines | |
| Ganine et al. | Transient aero-thermo-mechanical multidimensional analysis of a high pressure turbine assembly through a square cycle | |
| Zhou et al. | A loosely-coupled gas-kinetic BGK scheme for conjugate heat transfer in hypersonic flows |