西安理工大学学报
西安理工大學學報
서안리공대학학보
JOURNAL OF XI'AN UNIVERSITY OF TECHNOLOGY
2015年
1期
67-71
,共5页
阮辉%廖伟丽%黄永%赵亚萍%赵夏青
阮輝%廖偉麗%黃永%趙亞萍%趙夏青
원휘%료위려%황영%조아평%조하청
水翼%空化%噪声%数值模拟
水翼%空化%譟聲%數值模擬
수익%공화%조성%수치모의
hydrofoil%cavitation%noise%numerical simulation
以NACA0015水翼为研究对象,采用Schnerr‐Sauer空化模型和Ffowcs‐Wiliams & Hawk‐ing s声学模型,计算了二维水翼的空化噪声,并对水翼的空化过程和水翼空化的噪声性能进行了分析。研究结果表明,水翼空化呈现出明显的脉动性和周期性,空化空泡云脱落的周期为0.1704s,由漩涡引起的水翼壁面附近的反向射流是诱发空化空泡形成和脱落的主要成因。通过分析各个监测点的声压脉动特性可知,噪声在水翼头部区域的传播与主流方向一致,没有逆向传播。在空化发展过程中,空化区域的噪声信号有向下游叠加的趋势,但是传播到水翼尾部流动区域时,已经逐渐衰减完毕。
以NACA0015水翼為研究對象,採用Schnerr‐Sauer空化模型和Ffowcs‐Wiliams & Hawk‐ing s聲學模型,計算瞭二維水翼的空化譟聲,併對水翼的空化過程和水翼空化的譟聲性能進行瞭分析。研究結果錶明,水翼空化呈現齣明顯的脈動性和週期性,空化空泡雲脫落的週期為0.1704s,由漩渦引起的水翼壁麵附近的反嚮射流是誘髮空化空泡形成和脫落的主要成因。通過分析各箇鑑測點的聲壓脈動特性可知,譟聲在水翼頭部區域的傳播與主流方嚮一緻,沒有逆嚮傳播。在空化髮展過程中,空化區域的譟聲信號有嚮下遊疊加的趨勢,但是傳播到水翼尾部流動區域時,已經逐漸衰減完畢。
이NACA0015수익위연구대상,채용Schnerr‐Sauer공화모형화Ffowcs‐Wiliams & Hawk‐ing s성학모형,계산료이유수익적공화조성,병대수익적공화과정화수익공화적조성성능진행료분석。연구결과표명,수익공화정현출명현적맥동성화주기성,공화공포운탈락적주기위0.1704s,유선와인기적수익벽면부근적반향사류시유발공화공포형성화탈락적주요성인。통과분석각개감측점적성압맥동특성가지,조성재수익두부구역적전파여주류방향일치,몰유역향전파。재공화발전과정중,공화구역적조성신호유향하유첩가적추세,단시전파도수익미부류동구역시,이경축점쇠감완필。
With NACA0015 hydrofoil as the research objective ,Schnerr‐Sauer hydrofoil model and Ffowes‐Wiliams & Hawkings acoustic models are adopted to calculate the two‐dimensional hydrofoil cavitation noises and to analyze the performances of hydrofoil cavitation process and hy‐drofoil cavitation noises .T he research results indicate that hydrofoil cavitation process appears to have obvious pulsation and periodicity ,and that the period of cavitation cloud falling off is 0 .170 4 s .The reverse jet induced by the vortex near the wall of hydrofoil is the major cause of cavitati‐on inception and falling off .T he transmission direction of noise in the head of hydrofoil is the same with the main flow direction ,and backward transmission does not happen .In the process of cavitation development ,the noise signal of cavitation region has the tendency of adding to dow n‐stream ,but w hen the noise signal spreads to the hydrofoil tail for region ,it has gradually attenu‐ated .