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Newsletter  2023.10  Index

Theme : "AJK FED 2023"

  1. Preface
    Hyun Jin PARK, Shoichi MATSUDA, Chungpyo HONG
  2. Evaluation of railway vehicles' resistance against strong crosswinds and its application for safe railway operation
    Yayoi MISU (East Japan Railway Company)
  3. Order within Turbulence
    Susumu GOTO (Osaka University), Yutaro MOTOORI (Osaka University)
  4. LES/Lagrangian-particle-simulation of a Reactive Turbulent Planar Jet
    Jiabao Xing (Nagoya University),Tomoaki WATANABE (Nagoya University),and Koji NAGATA (Kyoto University)
  5. Unsteady Characteristics of Tip Leakage Vortex Cavitation in the Occurrence of Cavitation Instability in Liquid Rocket Inducer
    Koki TAMURA (Tohoku University),Yuto NAKURA (Tohoku University), Satoshi KAWASAKI (Japan Aerospace Exploration Agency), Yuka IGA (Tohoku University)
  6. Water Condensation in PEMFCs at Nano-scale: Insights through Lattice DFT simulations
    Clint John Cortes OTIC (The University of Tokyo), Masazumi ARAO (FC-Cubic), Masashi MATSUMOTO (FC-Cubic), Hideto IMAI (FC-Cubic), Ikuya KINEFUCHI (The University of Tokyo)
  7. Reconstruction of Fluid Stress Field from Flow Birefringence using Physics-Informed Convolutional Encoder-Decoder (PICED)
    Daichi IGARASHI (Tokyo University of Agriculture and Technology), Shun MIYATAKE (Tokyo University of Agriculture and Technology), Jingzu YEE (Tokyo University of Agriculture and Technology), Yoshiyuki TAGAWA (Tokyo University of Agriculture and Technology)
  8. Determination of Permeability in the Volume Penalisation Method with a Smooth Mask Function
    Taichi TSUJIMOTO (Osaka University), Yuta NAKAO (Osaka University), Takuya TSUJI (Osaka University), Toshitsugu TANAKA (Osaka University), Kimiaki WASHINO (Osaka University)

 

Unsteady Characteristic of Tip Leakage Vortex Cavitation in the Occurrence of Cavitation Instability in Inducer


Koki TAMURA
Tohoku University,

Yuto NAKURA
Tohoku University,

Satoshi KAWASAKI
Japan Aerospace Exploration Agency,

Yuka IGA
Tohoku University

Abstract

Cavitation is a phase change phenomenon from liquid to gas that occurs in the low-pressure region of high-speed fluid machinery. In liquid rocket inducer, the tip leakage vortex cavitation (T.L.V.C.) is the primary occurrence, and unsteady oscillation of T.L.V.C. causes pump unstable, called cavitation instability. This instability frequently encountered during the development of the turbopump. Therefore, it is crucial to elucidate the unsteady characteristics of T.L.V.C. as a cause of cavitation instability. The present study focuses on T.L.V.C. arising in the inducer, with particular emphasis on cavity length. Additionally, the fundamental characteristics of T.L.V.C. arising in NACA0009 hydrofoil with tip clearance is also examined to consider the characteristics of T.L.V.C. in the inducer.

The tested inducer and hydrofoil are depicted in Fig. 1 and 2. Cavitation was visualized to determine the cavity length and frequency of cavity oscillation in both experiments, and the Strouhal number based on cavity length () was calculated.

In the inducer experiment, it was found that the characteristic of  of T.L.V.C. in the occurrence of cavitation surge (C.S.) differ from that of T.L.V.C. in super-synchronous rotating cavitation (super-S R.C.). The result of  in super-S R.C. at the beginning to the middle is consistence with that of T.L.V.C. arising in the hydrofoil. However, the characteristic of  of T.LV.C. at the end of super-S R.C. showed a different trend than before. Assuming that the characteristic of  of T.L.V.C. arising in the hydrofoil represents the natural oscillation characteristic of T.L.V.C., the T.L.V.C. at the beginning to the middle of super-S R.C. oscillate naturally. Subsequently super-S R.C. ended when the T.L.V.C. become less prone to oscillation and starts transitioning to different mode of oscillation. In contrast, the T.L.V.C. in the occurrence of C.S., which has different characteristic of  from T.L.V.C. arising in hydrofoil, oscillates unnaturally.

Key words

Rotating Cavitation, Cavitation Surge, Tip Leakage Vortex Cavitation, Inducer, NACA0009

Figures


Fig. 1       Tested inducer (THK inducer).


Fig. 2        Tested hydrofoil (NACA0009).

Last Update:10.13.2023