Pyrolysis and Chemical Ablation Analysis of Hypersonic Missile for Thermal Protection Design Applying Charring Phenol Resin Composites
A chemical ablation analysis of hypersonic missile for thermal protection design was performed using SAMCEF AMARYLLIS V.17, the specific ablation module of commercial software based on a finite element code. The pyrolysis and surface recession models based on the effects of mass loss, pore gas diffu...
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| 主要な著者: | , , , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
Korean Society for Precision Engineering
2018-10-01
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| シリーズ: | 한국정밀공학회지 |
| 主題: | |
| オンライン･アクセス: | http://jkspe.or.kr/upload/pdf/NODE07537850.pdf |
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