SINGLE-LAYER MARCHING ALGORITHM TO CALCULATE SUPERSONIC FLOW ABOUT ROCKETS WITH THE COMPUTATIONAL REGION DIVIDED INTO SEVERAL SUBREGIONS
This paper presents a single-layer marching algorithm to calculate supersonic flow about rockets that may be equipped with wings, stabilizers, rudders, and superstructures. In this algorithm, the rocket along its axis is divided into sections of two types: sections along the rocket structure without...
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| Datum: | 2025 |
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| Format: | Artikel |
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текст 3
2025
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| Online Zugang: | https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/152 |
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| Назва журналу: | Technical Mechanics |