Application of the DRBEM to model ablation characteristics of a thrust vector control vane. (English) Zbl 0973.76064
From the summary: A dual reciprocity boundary element method (DRBEM) is implemented to predict ablation in model thrust vector control vanes. A moving front algorithm is described. Numerical results for recession of quarter-scale and half-scale vanes compare well with experimental data.
MSC:
| 76M15 | Boundary element methods applied to problems in fluid mechanics |
| 76T99 | Multiphase and multicomponent flows |
Keywords:
dual reciprocity boundary element method; ablation; thrust vector control vanes; moving front algorithmReferences:
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