Ferraiuolo et al., 2009 - Google Patents
Thermostructural design of a flying winglet experimental structure for the EXPERT re-entry testFerraiuolo et al., 2009
View PDF- Document ID
- 2870644613189132871
- Author
- Ferraiuolo M
- Riccio A
- Gigliotti M
- Tescione D
- Gardi R
- Marino G
- Publication year
External Links
Snippet
Within the framework of the European Experimental Re-entry Test Bed (EXPERT) Program, aimed at improving the understanding of physical phenomena occurring during the return of space vehicles from space to earth, the design of a flying winged experimental payload has …
- 230000035882 stress 0 abstract description 51
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
- G06F17/5086—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]
- G06F2217/80—Thermal analysis and optimization
-
- 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
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Zhang et al. | Time-adaptive, loosely coupled strategy for conjugate heat transfer problems in hypersonic flows | |
| Lamorte et al. | Uncertainty propagation in integrated airframe–propulsion system analysis for hypersonic vehicles | |
| Weng et al. | Numerical investigation of thermal response using orthotropic charring ablative material | |
| Ji et al. | Investigation on thermal performance of high temperature multilayer insulations for hypersonic vehicles under aerodynamic heating condition | |
| Peng et al. | Generalized free-edge stress analysis using mechanics of structure genome | |
| Chen et al. | Multidimensional finite volume fully implicit ablation and thermal response code | |
| Cross et al. | Two-dimensional modeling of ablation and pyrolysis with application to rocket nozzles | |
| Carrera et al. | Aeroelastic analysis of pinched panels in supersonic flow changing with altitude | |
| Xie et al. | Optimization design and analysis of multilayer lightweight thermal protection structures under aerodynamic heating conditions | |
| Medeiros et al. | Computational aeroelasticity using modal-based structural nonlinear analysis | |
| Ostoich et al. | Fluid-thermal response of spherical dome under a mach 6.59 laminar boundary layer | |
| Xie et al. | Thermal and thermomechanical performances of pyramidal core sandwich panels under aerodynamic heating | |
| Chen et al. | Loosely coupled simulation for two-dimensional ablation and shape change | |
| Cheng et al. | Effects of radiation heating on modal characteristics of panel structures | |
| Ejtehadi et al. | Full continuum approach for simulating plume-surface interaction in planetary landings | |
| Zhu et al. | Study on helium impingement cooling for a sharp leading edge subject to aerodynamic heating | |
| Lei et al. | Experimental model design and preliminary numerical verification of fluid–thermal–structural coupling problem | |
| Wright et al. | An overview of technology investments in the NASA entry systems modeling project | |
| Brune et al. | Uncertainty analysis of fluid-structure interaction of a deformable hypersonic inflatable aerodynamic decelerator | |
| Ferraiuolo et al. | Thermostructural design of a flying winglet experimental structure for the EXPERT re-entry test | |
| Votta et al. | Hypersonic low-density aerothermodynamics of Orion-like exploration vehicle | |
| Iwasa | Wrinkle-reduction law for rectangular membranes under a shear load | |
| Goldberg | Hypersonic flow heat transfer prediction using single equation turbulence models | |
| Capra et al. | Aerothermal–Structural Analysis of a Rocket-Launched Mach 8 Scramjet Experiment: Descent | |
| Thawait et al. | Delayed detached eddy simulation-based aerothermoelastic analysis of deployable control fin in supersonic and hypersonic flows |