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The Schlieren as well as oil flow experimental results are presented for Mach 2 flow. Numerical solutions of fluid flow over the spinning cone are performed in transient case as well as steady case using commercially available Ansys Fluent. The effect of spin on local wall pressure, local skin friction, local wall adjacent temperature as well as heat flux are quantified at Mach 2 flow. The transient velocity contour around spinning cone at still fluid case is presented.

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Unsteady Numerical Studies on Spinning Cone at Different Flow Regimes

  • 会议论文

  • 发表日期：

    2025年

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  • Rajkamal Sah,
  • Sathia Narayanan,
  • L. Venkatakrishnan,
  • Gopalan Jagadeesh

摘要

The Schlieren as well as oil flow experimental results are presented for Mach 2 flow. Numerical solutions of fluid flow over the spinning cone are performed in transient case as well as steady case using commercially available Ansys Fluent. The effect of spin on local wall pressure, local skin friction, local wall adjacent temperature as well as heat flux are quantified at Mach 2 flow. The transient velocity contour around spinning cone at still fluid case is presented.