原文传递
Sensitivity of Space Launch System Low-Speed Aerodynamic CFD Results to Kestrel Flow Solver Inputs.
| 题名： | Sensitivity of Space Launch System Low-Speed Aerodynamic CFD Results to Kestrel Flow Solver Inputs. |
| 作者： | Pomeroy, B. W; Krist, S. E; Wignall, T. J. |
| 摘要： | Within the Space Launch System (SLS) program, the Kestrel flow solver has be- come the tool of choice for conducting aerodynamic simulations for the low-speed liftoff and transition flight regimes. Despite having used Kestrel to develop transition regime lineload databases for four SLS configurations, the uncertainty in these databases has yet to be established, primarily due to the large computational re- sources required for each simulation and the large number of simulations required to construct the uncertainty bounds. En route to formulating such bounds, an assessment of the sensitivity of the simulations to variations in the settings of the flow solver input parameters is essential. Accordingly, a comprehensive study of perturbations to the input settings, for a single flow condition, has been conducted; results were processed with the goals of pinpointing the regions of the flow most sensitive to the various input settings, quantifying input setting effects on key aerodynamic characteristics, and providing a first look at the magnitude of the uncertainty in the lineloads. |
| 总页数： | 112 pages |
相关文献
- NASA's Space Launch System Moves into Testing and Integration.
- Management and Analysis of Michigan Intelligent Transportation Systems Center Data with application to the Detroit Area I-75 Corridor.
- The Design and Development of a Low-Speed, Low-Force Wind Tunnel Data Acquisition System With an Application to Bicycle Front Fork Spacing.
- Comparison of Computed and Measured Vortex Evolution for a UH-60A Rotor in Forward Flight.
- Investigating the Sensitivity of Optimal Network Safety Needs to Key Safety Management Inputs.
- NASA's Space Launch System: Deep-Space Opportunities for Smallsats.
检索历史
应用推荐
