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頁籤選單縮合
題 名 | Design of the Divergent Portion of a Two-Dimensional Supersonic Nozzle |
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作 者 | 仲偉浩; 林文賓; | 書刊名 | 黃埔學報 |
卷 期 | 40 2001.01[民90.01] |
頁 次 | 頁357-365 |
分類號 | 440.137 |
關鍵詞 | 超音速流; 噴嘴; Supersonic flow; Nozzle; Mach number; Shock wave; Euler equation; |
語 文 | 英文(English) |
英文摘要 | The nozzle for supersonic flow is designed in this paper such that it is of minimum length, flow at the exit is uniform and parallel to the centerline of the nozzle, the flow within the nozzle is shock free, and the Mach number at exit equals the desired one. Based on these principles, contour lines representing the wall of the divergent portion of the nozzle are plotted, enabling the evaluation of nozzle lengths which depend on the Mach number. Comparisons between numerical and analytical solutions are made to assure the accuracy of computations. |
本系統中英文摘要資訊取自各篇刊載內容。