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研究生:王昌楠
研究生(外文):Wang, Chang-Nan
論文名稱:不足膨脹噴流與空穴交互作用下震波振盪流場之實驗研究
論文名稱(外文):Experimental Study on the Shock Oscillating in an Underexpanded Jet to Cavity Interaction Flow
指導教授:尤芳忞
指導教授(外文):Fang-Min Yu
學位類別:碩士
校院名稱:國立成功大學
系所名稱:航空太空工程學系
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:1997
畢業學年度:85
語文別:中文
論文頁數:99
中文關鍵詞:震波振盪不足膨脹噴流噴嘴
外文關鍵詞:shock oscillatingunderexpanded jetnozzle
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不足膨脹噴流與空穴管正向交互作用下,選定穴管長、噴嘴至空穴口
間距、噴嘴全壓比作為參數來觀測管內壓力振盪的情形。管內的流場主要
有吞吐式及尖聲式兩種,主要差別在於噴嘴全壓比及噴嘴至空穴口之間距
,而其理論以前人的共振管流體動力學來作說明。從本實驗中知,空穴管
內的壓力波振盪主頻均接近理論的基頻或其基頻的數倍呈現,且在特殊條
件下壓力波的振幅達至70psi,此時其主頻以低於基頻出現而穴管底溫度
也在此條件下升高。因壓力波之振幅產生的熵留在穴管底部並累積造成管
底溫度的提升。本實驗也以開口管及以海綿為底做比較,其中開放管因無
底端作反射所以並沒有明顯的壓力振盪產生,而海綿為底的穴管內雖有壓
力振盪但因壓力波至管底時能量被海綿吸收故其振盪振幅極微。

Underexpansion jet to cavity flow induced pressure
oscillation inside the cavity tube and the induced temperature
increasing on the bottom of the tube has been investigated based
on three parameters of nozzle pressure ratio, nozzle exit to
cavity distance and the cavity tube length. Two major flow modes
named as regurgitant mode and screeching mode were observed. The
measured major frequency on the pressure oscillation inside
cavity tube is very closed to the theoretical fundamental
frequency of the flow system or its multiplier. Instead of a
solid cavity tube end, as replacing it with a sponge-end or a
open-end, it has been observed that the amplitude of the
pressure oscillating reduced to a negligible level, however, the
major frequency remains on the same characteristics. It is
concluded that the major mechanism for the pressure oscillating
inside cavity tube is owing to the pressure wave reflection
between the solid end surface and the inlet surface of the
cavity tube. On some regurgitant modes the amplitude of the
pressure oscillation can be as high as 70 psia, with a frequency
closed to the fundamental frequency. Due to the accumulation of
the entropy on the cavity tube end on the pressure oscillation
processes in regurgitant mode, an obviously temperature rising
has been measured on the end of the cavity tube.

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