• 대한조선학회논문집
• /
• 제30권4호
• /
• pp.46-60
• /
• 1993

캐비테이션 터널에서 변동압력의 정확한 계측은 실선에서의 진동과 소음세기 예측에 필요하다. 본문에서는 프로펠러 케비테이션에 의해 야기되는 변동압력의 실험적연구 결과를 나타내고 논의 한다. 문제시 되고 있는 프로펠러 회전수에 의한 영향을 이해하고자 변동압력을 캐비테이션 터널에서 평판을 이용하여 여러 회전수에서 계측 하였다. 균일류에서 오차를 추정하기 위하여 계측 및 계측결과에서의 불확실성 해석이 사용 되었다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
• /
• pp.333-339
• /
• 2003

Steady and unsteady cavitation characteristics of turbopump inducer were investigated in this paper. To see the effect of blade angle on the inducer performance, three inducers with inlet tip blade angle of $7.8^{\circ},\;7.0^{\circ},\;6.1^{\circ}$, respectively, were tested. For $7.8^{\circ},\;7.0^{\circ}$ inducers in the non-cavitating condition, head decreased linearly with flow rate, but head-flow rate curve had a dip at the flow coefficient ${\Phi}=0.065\;for\;6.1^{\circ}$ inducer. Rotating cavitation and cavitation surge were found in the $7.8^{\circ},\;7.0^{\circ}$ inducers in the cavitation tests. During the rotating cavitation one cell rotated at the same rotational speed as that of the inducer. The cavitation surge did not rotate and the oscillating frequency was $7{\sim}20\;Hz$. From the curve of the critical cavitation number versus flow rate, it was found that the steady cavitation performance of $6.1^{\circ}$ inducer was much lower than that of $7.8^{\circ},\;7.0^{\circ}$ inducers.